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New Crowdin translations - uk (#26432)
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@@ -179,6 +179,7 @@
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- [CubePilot Cube Orange (CubePilot)](flight_controller/cubepilot_cube_orange.md)
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- [CubePilot Cube Yellow (CubePilot)](flight_controller/cubepilot_cube_yellow.md)
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- [Швидке підключення Cube](assembly/quick_start_cube.md)
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- [Gear Up AirBrainH743](flight_controller/gearup_airbrainh743.md)
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- [Holybro Kakute H7v2](flight_controller/kakuteh7v2.md)
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- [Holybro Kakute H7mini](flight_controller/kakuteh7mini.md)
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- [Holybro Kakute H7](flight_controller/kakuteh7.md)
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@@ -255,7 +256,7 @@
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- [Benewake TFmini Lidar](sensor/tfmini.md)
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- [LeddarOne Lidar](sensor/leddar_one.md)
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- [Lidar-Lite](sensor/lidar_lite.md)
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- [Lightware Lidars (SF/LW)](sensor/sfxx_lidar.md)
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- [Lightware Lidars (SF/LW/GRF)](sensor/sfxx_lidar.md)
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- [Lightware SF45 Rotary Lidar](sensor/sf45_rotating_lidar.md)
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- [TeraRanger](sensor/teraranger.md)
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- [✘ Lanbao PSK-CM8JL65-CC5](sensor/cm8jl65_ir_distance_sensor.md)
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@@ -932,6 +933,7 @@
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- [Ліцензії](contribute/licenses.md)
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- [Релізи](releases/index.md)
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- [Release Process](releases/release_process.md)
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- [main (alpha)](releases/main.md)
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- [1.17 (alpha)](releases/1.17.md)
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- [1.16 (stable)](releases/1.16.md)
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@@ -12,19 +12,16 @@ The [ARK Jetson Pixhawk Autopilot Bus (PAB) Carrier](https://arkelectron.gitbook
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## Характеристики
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- **Power Requirements**
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- 5V
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- 4A minimum (dependent on usage and peripherals)
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- **Additional Features**
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- Pixhawk Autopilot Bus (PAB) Form Factor ([PAB Standard](https://github.com/pixhawk/Pixhawk-Standards/blob/master/DS-010%20Pixhawk%20Autopilot%20Bus%20Standard.pdf))
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- Слот MicroSD
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- USA-built, NDAA compliant
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- Integrated 1W heater for sensor stability in extreme conditions
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- **Physical Details**
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- Weight:
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- Without Jetson and Flight Controller – 80g
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- With Jetson, no heatsink or Flight Controller – 108g
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@@ -170,7 +170,6 @@ FC повинен бути налаштований для підключенн
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2. [Встановіть параметри](../advanced_config/parameters.md):
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- `MAV_1_CONFIG` = `102`
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- `MAV_1_MODE = 2`
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- `SER_TEL2_BAUD` = `921600`
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@@ -184,7 +183,6 @@ FC повинен бути налаштований для підключенн
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1. Connect to the RPi (using WiFi, a router, or a WiFi Dongle).
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2. Увімкніть послідовний порт RPi, запустивши `RPi-config`
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- Перейдіть до `3 Варіанти інтерфейсу`, потім `I6 Серійний порт`.
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Потім введіть:
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- `login shell accessible over serial → No`
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@@ -145,7 +145,6 @@ make px4_fmu-v6c_default upload
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```
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3. Перейдіть до **Варіанти інтерфейсу**, а потім клацніть **Серійний порт**.
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- Виберіть **No**, щоб вимкнути послідовний вхід у оболонку.
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- Виберіть **Так**, щоб увімкнути послідовний інтерфейс.
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- Клацніть **Завершити** та перезапустіть RPi.
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@@ -164,7 +163,6 @@ make px4_fmu-v6c_default upload
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```
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6. Далі збережіть файл і перезапустіть RPi.
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- У `nano` ви можете зберегти файл за допомогою такої послідовності комбінацій клавіш: **ctrl+x**, **ctrl+y**, **Enter**.
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7. Перевірте, чи доступний послідовний порт.
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@@ -214,7 +214,6 @@ The Lua script works by extracting the `obstacle_distance_fused` data at each ti
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3. Open PlotJuggler and navigate to the **Tools > Reactive Script Editor** section.
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In the **Script Editor** tab, add following scripts in the appropriate sections:
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- **Global code, executed once:**
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```lua
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@@ -33,7 +33,6 @@ _Польотні завдання_ використовуються у [Реж
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- FlightTaskMyTask.cpp
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3. Оновіть **CMakeLists.txt** для нового завдання
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- Скопіюйте вміст **CMakeLists.txt** з іншого завдання, наприклад, [Orbit/CMakeLists.txt](https://github.com/PX4/PX4-Autopilot/blob/main/src/modules/flight_mode_manager/tasks/Orbit/CMakeLists.txt)
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- Оновіть відмітку про авторське право до поточного року
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@@ -84,16 +84,9 @@ The RC sticks cannot be used during autotuning (moving the sticks will stop the
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If an [Enable/Disable Autotune Switch](#enable-disable-autotune-switch) is configured you can just toggle the switch to the "enabled" position.
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</div></div>
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1. In QGroundControl, open the menu **Vehicle setup > PID Tuning**:
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2. Select either the _Rate Controller_ or _Attitude Controller_ tabs.
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3. Ensure that the **Autotune enabled** button is enabled (this will display the **Autotune** button and remove the manual tuning selectors).
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4. Read the warning popup and click on **OK** to start tuning.
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 2. Select either the _Rate Controller_ or _Attitude Controller_ tabs. 3. Ensure that the **Autotune enabled** button is enabled (this will display the **Autotune** button and remove the manual tuning selectors). 4. Read the warning popup and click on **OK** to start tuning.
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<div style="display: inline;" v-if="$frontmatter.frame === 'Multicopter'">
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@@ -22,7 +22,6 @@ Performing this calibration step is only recommended if the autopilot's orientat
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:::
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4. Помістіть транспортний засіб на рівну відстань на рівній поверхні:
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- Для літаків це положення під час рівнопланового польоту (літаки мають тенденцію трохи підняти свої крила!)
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- Для коптерів це позиція утримання.
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@@ -281,7 +281,7 @@ Acting on a detected failure during flight is deactivated by default (enable by
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During **takeoff** the failure detector [attitude trigger](#attitude-trigger) invokes the [disarm action](#act_disarm) if the vehicle flips (disarm kills the motors but, unlike flight termination, will not launch a parachute or perform other failure actions).
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Note that this check is _always enabled on takeoff_, irrespective of the `CBRK_FLIGHTTERM` parameter.
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The failure detector is active in all vehicle types and modes, except for those where the vehicle is _expected_ to do flips (i.e. [Acro mode (MC)](../flight_modes_mc/altitude.md), [Acro mode (FW)](../flight_modes_fw/altitude.md), and [Manual (FW)](../flight_modes_fw/manual.md)).
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The failure detector is active in all vehicle types and modes, except for those where the vehicle is _expected_ to do flips (i.e. [Acro mode (MC)](../flight_modes_mc/acro.md), [Acro mode (FW)](../flight_modes_fw/acro.md), and [Manual (FW)](../flight_modes_fw/manual.md)).
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### Тригер висоти
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@@ -77,7 +77,6 @@ This section contains topics related to [helicopter](../frames_helicopter/index.
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3. Видаліть лопаті ротора та пропелери
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4. Assign motors and servos to outputs and test (also in [Actuator configuration](../config/actuators.md)):
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1. Assign the [motors and servos to the outputs](../config/actuators.md#actuator-outputs).
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2. Power the vehicle with a battery and use the [actuator testing sliders](../config/actuators.md#actuator-testing) to validate correct servo and motor assignment and direction.
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@@ -140,7 +140,6 @@ Make sure to have assigned a [Kill switch](../config/safety.md#emergency-switche
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13. Повторіть процес налаштування контролера нахилу для всіх осей.
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14. Повторіть процес налаштування контролерів швидкості та позицій (на всіх осях).
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- Використовуйте режим позиції при налаштуванні цих контролерів
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- Select the **Simple position control** option in the _Position control mode ..._ selector (this allows direct control for the generation of step inputs)
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@@ -18,28 +18,37 @@ A drive mode will only work properly if all the configuration for the preceding
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## Flashing the Rover Build
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Rovers use a custom build that must be flashed onto your flight controller instead of the default PX4 build:
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Rover is built as a [firmware variant](../dev_setup/building_px4.md#px4-make-build-targets), and must be installed as "Custom Firmware" in QGC (other vehicles are present in the default variant).
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1. First build the rover firmware for your flight controller from the `main` branch (there is no release build, so you can't just select this build from QGroundControl).
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The release versions of Rover firmware for different boards are attached to the associated GitHub release tag.
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For example, you can find `px4_fmu-v5x_rover.px4` on [PX4-Autopilot/releases/tag/v1.16.1](https://github.com/PX4/PX4-Autopilot/releases/tag/v1.16.1).
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For the `main` branch version of Rover you will need to [build the firmware](#building-rover).
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To build for rover with the `make` command, replace the `_default` suffix with `_rover`.
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For example, to build rover for px4_fmu-v6x boards, you would use the command:
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Load the firmware onto your flight controller as "Custom Firmware" (see [Loading Firmware > Installing PX4 Main, Beta or Custom Firmware](../config/firmware.md#installing-px4-main-beta-or-custom-firmware)).
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```sh
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make px4_fmu-v6x_rover
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```
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## Building Rover
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::: info
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You can also enable the modules in default builds by adding these lines to your [board configuration](../hardware/porting_guide_config.md) (e.g. for fmu-v6x you might add them to [`main/boards/px4/fmu-v6x/default.px4board`](https://github.com/PX4/PX4-Autopilot/blob/main/boards/px4/fmu-v6x/default.px4board)):
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Rover is built as the `rover` [firmware variant](../dev_setup/building_px4.md#px4-make-build-targets).
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What this means is that when building the firmware with the `make` command, you replace the `_default` suffix in the configuration target with `_rover`.
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```sh
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CONFIG_MODULES_ROVER_ACKERMANN=y
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CONFIG_MODULES_ROVER_DIFFERENTIAL=y
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CONFIG_MODULES_ROVER_MECANUM=y
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```
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For example, to build rover for `px4_fmu-v6x` boards, you would use the following command:
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Note that adding the rover modules may lead to flash overflow, in which case you will need to disable modules that you do not plan to use (such as those related to multicopter or fixed wing).
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```sh
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make px4_fmu-v6x_rover
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```
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Note that configuration targets are constructed with the format "VENDOR_MODEL_VARIANT".
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The built firmware can be installed as custom firmware, as shown above in in [Flashing the Rover Build](#flashing-the-rover-build).
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:::info
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You can also enable the modules in default builds by adding these lines to your [board configuration](../hardware/porting_guide_config.md) (e.g. for fmu-v6x you might add them to [`main/boards/px4/fmu-v6x/default.px4board`](https://github.com/PX4/PX4-Autopilot/blob/main/boards/px4/fmu-v6x/default.px4board)):
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```sh
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CONFIG_MODULES_ROVER_ACKERMANN=y
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CONFIG_MODULES_ROVER_DIFFERENTIAL=y
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CONFIG_MODULES_ROVER_MECANUM=y
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```
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Adding the rover modules may lead to flash overflow, in which case you will need to disable modules that you do not plan to use (such as those related to multicopter or fixed wing).
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:::
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2. Load the **custom firmware** that you just built onto your flight controller (see [Loading Firmware > Installing PX4 Main, Beta or Custom Firmware](../config/firmware.md#installing-px4-main-beta-or-custom-firmware)).
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@@ -307,7 +307,6 @@ If the airframe is for a **new group** you additionally need to:
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```
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3. Update _QGroundControl_:
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- Add the svg image for the group into: [src/AutopilotPlugins/Common/images](https://github.com/mavlink/qgroundcontrol/tree/master/src/AutoPilotPlugins/Common/Images)
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- Add reference to the svg image into [qgcimages.qrc](https://github.com/mavlink/qgroundcontrol/blob/master/qgcimages.qrc), following the pattern below:
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@@ -39,16 +39,6 @@ Navigate into the **PX4-Autopilot** directory and start [Gazebo SITL](../sim_gaz
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make px4_sitl gz_x500
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```
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:::details
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If you installed Gazebo Classic
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Start [Gazebo Classic SITL](../sim_gazebo_classic/index.md) using the following command:
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```sh
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make px4_sitl gazebo-classic
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```
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:::
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This will bring up the PX4 console:
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@@ -89,6 +79,16 @@ cd PX4-Autopilot
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make px4_fmu-v5_default
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```
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:::tip
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You can also build using the [px4-dev Docker container](../test_and_ci/docker.md) without installing the toolchain locally.
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From the PX4-Autopilot directory:
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```sh
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./Tools/docker_run.sh 'make px4_fmu-v5_default'
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```
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:::
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Успішне виконання виведе в консолі приблизно наступне в кінці:
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```sh
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@@ -145,7 +145,8 @@ The following list shows the build commands for the [Pixhawk standard](../flight
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- [Pixhawk 1 (FMUv2)](../flight_controller/pixhawk.md): `make px4_fmu-v2_default`
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:::warning
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You **must** use a supported version of GCC to build this board (e.g. the same as used by [CI/docker](../test_and_ci/docker.md)) or remove modules from the build. Збірка прошивки за допомогою компілятора GCC, який не підтримується може зазнати невдачі, оскільки обсяг памʼяті, який займає PX4, близький до ліміту пам'яті плати в 1 МБ.
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You **must** use a supported version of GCC to build this board (e.g. the `gcc-arm-none-eabi` package from the current Ubuntu LTS, which is the same toolchain used by CI) or remove modules from the build.
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Збірка прошивки за допомогою компілятора GCC, який не підтримується може зазнати невдачі, оскільки обсяг памʼяті, який займає PX4, близький до ліміту пам'яті плати в 1 МБ.
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:::
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@@ -211,7 +212,7 @@ The `region 'flash' overflowed by XXXX bytes` error indicates that the firmware
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This is common for `make px4_fmu-v2_default` builds, where the flash size is limited to 1MB.
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If you're building the _vanilla_ master branch, the most likely cause is using an unsupported version of GCC.
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In this case, install the version specified in the [Developer Toolchain](../dev_setup/dev_env.md) instructions.
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In this case, install the `gcc-arm-none-eabi` package from the current Ubuntu LTS as described in the [Developer Toolchain](../dev_setup/dev_env.md) instructions.
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If building your own branch, it is possible that you have increased the firmware size over the 1MB limit.
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В цьому випадку вам доведеться видалити всі не потрібні при цій збірці модулі та драйвера.
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@@ -224,7 +225,7 @@ MacOS дозволяє тримати за замовчуванням відкр
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The build toolchain will then report `Too many open files` for many files, as shown below:
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```sh
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/usr/local/Cellar/gcc-arm-none-eabi/20171218/bin/../lib/gcc/arm-none-eabi/7.2.1/../../../../arm-none-eabi/bin/ld: cannot find NuttX/nuttx/fs/libfs.a: Too many open files
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arm-none-eabi-ld: cannot find NuttX/nuttx/fs/libfs.a: Too many open files
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```
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Рішення полягає в збільшенні максимально дозволеної кількості відкритих файлів (наприклад, до 300).
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@@ -247,34 +248,9 @@ xcode-select --install
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sudo ln -s /Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/include/* /usr/local/include/
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```
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### Ubuntu 18.04: Помилки компіляції пов'язані з arm_none_eabi_gcc
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Build issues related to `arm_none_eabi_gcc`may be due to a broken g++ toolchain installation.
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Ви можете перевірити чи це так, перевіряючи чи є відсутні залежності:
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```sh
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arm-none-eabi-gcc --version
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arm-none-eabi-g++ --version
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arm-none-eabi-gdb --version
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arm-none-eabi-size --version
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```
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Приклад виводу bash з відсутніми залежностями:
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```sh
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arm-none-eabi-gdb --version
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arm-none-eabi-gdb: command not found
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```
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This can be resolved by removing and [reinstalling the compiler](https://askubuntu.com/questions/1243252/how-to-install-arm-none-eabi-gdb-on-ubuntu-20-04-lts-focal-fossa).
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### Ubuntu 18.04: "Visual Studio Code не може спостерігати за змінами в коді у великому робочому середовищі
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See [Visual Studio Code IDE (VSCode) > Troubleshooting](../dev_setup/vscode.md#troubleshooting).
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### Не вдалося імпортувати пакети Python
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"Failed to import" errors when running the `make px4_sitl jmavsim` command indicates that some Python packages are not installed (where expected).
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"Failed to import" errors when running the `make px4_sitl gz_x500` command indicates that some Python packages are not installed (where expected).
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```sh
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Failed to import jinja2: No module named 'jinja2'
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@@ -282,12 +258,12 @@ You may need to install it using:
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pip3 install --user jinja2
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```
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|
||||
Якщо ці залежності вже встановлені, це може бути тому, що на комп'ютері є декілька версій Python (наприклад Python 2.7.16, Python 3.8.3) і модуль не існує в версії, яка використовується в інструментарії збірки.
|
||||
If you have already installed these dependencies this may be because there is more than one Python version on the computer (e.g. Python 2.7.16 and Python 3.8.3), and the module is not present in the version used by the build toolchain.
|
||||
|
||||
Ви зможете виправити це явним чином встановивши залежності як показано:
|
||||
You should be able to fix this by installing the dependencies from the repository's requirements file:
|
||||
|
||||
```sh
|
||||
pip3 install --user pyserial empty toml numpy pandas jinja2 pyyaml pyros-genmsg packaging
|
||||
pip3 install --user -r Tools/setup/requirements.txt
|
||||
```
|
||||
|
||||
## Цілі збірки PX4
|
||||
|
||||
@@ -23,7 +23,7 @@ A Taranis RC and a mid-range Android tablet make a very inexpensive field kit.
|
||||
|
||||
- Lenovo Thinkpad with i5-core running Windows 11
|
||||
- MacBook Pro (early 2015 and later) with macOS 10.15 or later
|
||||
- Lenovo Thinkpad i5 with Ubuntu Linux 20.04 or later
|
||||
- Lenovo Thinkpad i5 with Ubuntu Linux 22.04 or later
|
||||
|
||||
- **Ground control station** (computer or tablet):
|
||||
- iPad (may require Wifi telemetry adapter)
|
||||
|
||||
@@ -2,7 +2,7 @@
|
||||
|
||||
The _supported platforms_ for PX4 development are:
|
||||
|
||||
- [Ubuntu Linux (24.04/22.04)](../dev_setup/dev_env_linux_ubuntu.md) — Recommended
|
||||
- [Ubuntu Linux (24.04/22.04)](../dev_setup/dev_env_linux_ubuntu.md)
|
||||
- [Windows (10/11)](../dev_setup/dev_env_windows_wsl.md) — via WSL2
|
||||
- [macOS](../dev_setup/dev_env_mac.md)
|
||||
|
||||
@@ -15,9 +15,9 @@ The _supported platforms_ for PX4 development are:
|
||||
| **NuttX based hardware:** [Pixhawk Series](../flight_controller/pixhawk_series.md), [Crazyflie](../complete_vehicles_mc/crazyflie2.md) | ✓ | ✓ | ✓ |
|
||||
| **Linux-based hardware:** [Raspberry Pi 2/3](../flight_controller/raspberry_pi_navio2.md) | ✓ | | |
|
||||
| **Simulation:** [Gazebo SITL](../sim_gazebo_gz/index.md) | ✓ | ✓ | ✓ |
|
||||
| **Simulation:** [Gazebo Classic SITL](../sim_gazebo_classic/index.md) | ✓ | ✓ | ✓ |
|
||||
| **Simulation:** [ROS with Gazebo Classic](../simulation/ros_interface.md) | ✓ | | ✓ |
|
||||
| **Simulation:** ROS 2 with Gazebo | ✓ | | ✓ |
|
||||
| **Simulation:** [Gazebo Classic SITL](../sim_gazebo_classic/index.md) | | ✓ | ✓ |
|
||||
| **Simulation:** [ROS with Gazebo Classic](../simulation/ros_interface.md) | | | ✓ |
|
||||
|
||||
Experienced Docker users can also build with the containers used by our continuous integration system: [Docker Containers](../test_and_ci/docker.md)
|
||||
|
||||
|
||||
@@ -39,8 +39,9 @@ You may want to also install `python-pip` and `screen`.
|
||||
Виконайте скрипт нижче для встановлення GCC 7-2017-q4:
|
||||
|
||||
:::warning
|
||||
This version of GCC is out of date.
|
||||
At time of writing the current version on Ubuntu is `9-2020-q2-update` (see [focal nuttx docker file](https://github.com/PX4/PX4-containers/blob/master/docker/Dockerfile_nuttx-focal#L28))
|
||||
This version of GCC is very outdated.
|
||||
PX4 now uses the `gcc-arm-none-eabi` package from the current Ubuntu LTS (GCC 13.2.1 on Ubuntu 24.04).
|
||||
This CentOS guide is community-maintained and may not produce working builds.
|
||||
:::
|
||||
|
||||
```sh
|
||||
|
||||
@@ -4,21 +4,14 @@ The following instructions use a bash script to set up the PX4 development envir
|
||||
|
||||
The environment includes:
|
||||
|
||||
- [Gazebo Simulator](../sim_gazebo_gz/index.md) ("Harmonic")
|
||||
- [Build toolchain for Pixhawk (and other NuttX-based hardware)](../dev_setup/building_px4.md#nuttx-pixhawk-based-boards).
|
||||
|
||||
On Ubuntu 22.04:
|
||||
|
||||
- [Gazebo Classic Simulator](../sim_gazebo_classic/index.md) can be used instead of Gazebo.
|
||||
Gazebo is nearing feature-parity with Gazebo-Classic on PX4, and will soon replace it for all use cases.
|
||||
- [Gazebo Simulator](../sim_gazebo_gz/index.md) (Gazebo Harmonic)
|
||||
- [Build toolchain for Pixhawk (and other NuttX-based hardware)](../dev_setup/building_px4.md#nuttx-pixhawk-based-boards) using the `gcc-arm-none-eabi` compiler from the Ubuntu package manager.
|
||||
|
||||
The build toolchain for other flight controllers, simulators, and working with ROS are discussed in the [Other Targets](#other-targets) section below.
|
||||
|
||||
:::details
|
||||
Can I use an older version of Ubuntu?
|
||||
PX4 supports the current and last Ubuntu LTS release where possible.
|
||||
Older releases are not supported (so you can't raise defects against them), but may still work.
|
||||
For example, Gazebo Classic setup is included in our standard build instructions for macOS, Ubuntu 18.04 and 20.04, and Windows on WSL2 for the same hosts.
|
||||
:::info
|
||||
PX4 targets the **current Ubuntu LTS** (24.04) for CI and release builds, with the **previous LTS** (22.04) also supported.
|
||||
Older Ubuntu versions are not supported and may not work.
|
||||
:::
|
||||
|
||||
## Симуляція та NuttX (Pixhawk)
|
||||
@@ -52,9 +45,7 @@ The script is intended to be run on _clean_ Ubuntu LTS installations, and may no
|
||||
- При появі підказки по ходу виконання скрипту підтвердить вибір.
|
||||
- You can use the `--no-nuttx` and `--no-sim-tools` options to omit the NuttX and/or simulation tools.
|
||||
|
||||
3. If you need Gazebo Classic (Ubuntu 22.04 only) then you can manually remove Gazebo and install it by following the instructions in [Gazebo Classic > Installation](../sim_gazebo_classic/index.md#installation).
|
||||
|
||||
4. Перезавантажте комп'ютер при завершенні.
|
||||
3. Перезавантажте комп'ютер при завершенні.
|
||||
|
||||
:::details
|
||||
Additional notes
|
||||
@@ -63,10 +54,11 @@ These notes are provided "for information only":
|
||||
- This setup is supported by the PX4 Dev Team.
|
||||
Інструкції також можуть працювати на інших системах заснованих на Debian Linux.
|
||||
|
||||
- You can verify the NuttX installation by confirming the `gcc` version as shown:
|
||||
- You can verify the NuttX installation by confirming `gcc` is available.
|
||||
The version depends on your Ubuntu release (e.g. GCC 13.2.1 on Ubuntu 24.04):
|
||||
|
||||
```sh
|
||||
$arm-none-eabi-gcc --version
|
||||
$ arm-none-eabi-gcc --version
|
||||
|
||||
arm-none-eabi-gcc (15:13.2.rel1-2) 13.2.1 20231009
|
||||
Copyright (C) 2023 Free Software Foundation, Inc.
|
||||
|
||||
@@ -61,20 +61,20 @@ The approach is similar to installing PX4 in your _own_ virtual machine, as desc
|
||||
wsl --install
|
||||
```
|
||||
|
||||
- Ubuntu 20.04 ([Gazebo-Classic Simulation](../sim_gazebo_classic/index.md))
|
||||
|
||||
```sh
|
||||
wsl --install -d Ubuntu-20.04
|
||||
```
|
||||
|
||||
- Ubuntu 22.04 ([Gazebo Simulation](../sim_gazebo_gz/index.md))
|
||||
|
||||
```sh
|
||||
wsl --install -d Ubuntu-22.04
|
||||
```
|
||||
|
||||
- Ubuntu 24.04 ([Gazebo Simulation](../sim_gazebo_gz/index.md))
|
||||
|
||||
```sh
|
||||
wsl --install -d Ubuntu-24.04
|
||||
```
|
||||
|
||||
::: info
|
||||
You can also install[Ubuntu 20.04](https://www.microsoft.com/store/productId/9MTTCL66CPXJ) and [Ubuntu 22.04](https://www.microsoft.com/store/productId/9PN20MSR04DW) from the store, which allows you to delete the application using the normal Windows Add/Remove settings:
|
||||
You can also [Ubuntu 24.04](https://www.microsoft.com/store/productId/9nz3klhxdjp5) or [Ubuntu 22.04](https://www.microsoft.com/store/productId/9PN20MSR04DW) from Microsoft Store, which allows you to delete the application using the normal Windows Add/Remove settings.
|
||||
|
||||
:::
|
||||
|
||||
@@ -110,7 +110,7 @@ If you're using [Windows Terminal](https://learn.microsoft.com/en-us/windows/ter
|
||||
```
|
||||
|
||||
```sh
|
||||
wsl -d Ubuntu-20.04
|
||||
wsl -d Ubuntu-24.04
|
||||
```
|
||||
|
||||
If you only have one version of Ubuntu, you can just use `wsl`.
|
||||
|
||||
@@ -61,7 +61,6 @@ You must already have installed the command line [PX4 developer environment](../
|
||||
Для збірки:
|
||||
|
||||
1. Оберіть свою ціль збірки ("cmake build config"):
|
||||
|
||||
- The current _cmake build target_ is shown on the blue _config_ bar at the bottom (if this is already your desired target, skip to next step).
|
||||

|
||||
|
||||
@@ -133,10 +132,10 @@ In order for the code completion to work (and other IntelliSense magic) you need
|
||||
|
||||
Цей розділ включає вказівки для помилок з налаштування та збірки.
|
||||
|
||||
### Ubuntu 18.04: "Visual Studio Code не може спостерігати за змінами в коді у великому робочому середовищі"
|
||||
### "Visual Studio Code is unable to watch for file changes in this large workspace"
|
||||
|
||||
Ця помилка з'являється при старті.
|
||||
On some systems, there is an upper-limit of 8192 file handles imposed on applications, which means that VSCode might not be able to detect file modifications in `/PX4-Autopilot`.
|
||||
On some systems, there is an upper-limit on file handles imposed on applications, which means that VSCode might not be able to detect file modifications in `/PX4-Autopilot`.
|
||||
|
||||
Ви можете збільшити цей ліміт, щоб уникнути помилки, коштом споживання пам'яті.
|
||||
Follow the [instructions here](https://code.visualstudio.com/docs/setup/linux#_visual-studio-code-is-unable-to-watch-for-file-changes-in-this-large-workspace-error-enospc).
|
||||
|
||||
@@ -100,7 +100,6 @@ In order to use dual ZED-F9P GPS heading in PX4, follow these steps:
|
||||
3. Components should be visible on the left panel.
|
||||
Click on the first `_Component_<ID#>` that maps to the ZED-F9P DroneCAN node (below shown as _Component 124_).
|
||||
4. Click on the _GPS_ subsection and configure the parameters listed below:
|
||||
|
||||
- `GPS_TYPE`: Either set to `17` for moving baseline _base_, or set to `18` to be the moving baseline _rover_.
|
||||
One F9P MUST be _rover_, and the other MUST be _base_.
|
||||
- `GPS_AUTO_CONFIG`: set to 1 for both the rover and base
|
||||
|
||||
@@ -39,12 +39,10 @@ The ESC comes in variants without connectors that you can solder in place, and a
|
||||
- 10 Pin JST-SH Debug
|
||||
|
||||
- Motor & Battery Connectors (with-connector version)
|
||||
|
||||
- MR30 Connector Limit Per Motor: 30A Continuous, 40A Burst
|
||||
- Four MR30 Motor Connectors
|
||||
|
||||
- Dimensions (with connectors)
|
||||
|
||||
- Size: 77.00mm x 42.00mm x 9.43mm
|
||||
- Mounting Pattern: 30.5mm
|
||||
- Weight: 24g
|
||||
|
||||
@@ -26,7 +26,6 @@ AIRLink має два комп'ютери та інтегрований LTE-мо
|
||||
## Характеристики
|
||||
|
||||
- **Sensors**
|
||||
|
||||
- 3x акселерометри, 3x гіроскопи, 3x магнітометри, 3x датчики тиску
|
||||
- ГНСС, далекоміри, лідари, оптичний потік, камери
|
||||
- 3x-кратне резервування IMU
|
||||
@@ -34,7 +33,6 @@ AIRLink має два комп'ютери та інтегрований LTE-мо
|
||||
- Стабілізація температури
|
||||
|
||||
- **Flight Controller**
|
||||
|
||||
- STM32F7, ARM Cortex M7 з FPU, 216 МГц, 2 МБ Flash, 512 кБ оперативної пам'яті
|
||||
- STM32F1, співпроцесор вводу/виводу (IO)
|
||||
- Ethernet, 10/100 Мбіт/с
|
||||
@@ -51,7 +49,6 @@ AIRLink має два комп'ютери та інтегрований LTE-мо
|
||||
- Запобіжний вимикач / LED опція
|
||||
|
||||
- **AI Mission Computer**
|
||||
|
||||
- 6-ядерний процесор: двоядерний Cortex-A72 + чотирьохядерний Cortex-A53
|
||||
- Графічний процесор Mali-T864, OpenGL ES1.1/2.0/3.0/3.1
|
||||
- VPU з декодуванням 4K VP8/9, 4K 10bits H265/H264 60fps
|
||||
@@ -65,7 +62,6 @@ AIRLink має два комп'ютери та інтегрований LTE-мо
|
||||
- 2х Video: 4-смугова MIPI CSI (FPV-камера) та 4-смугова MIPI CSI з входом HMDI (камера корисного навантаження)
|
||||
|
||||
- **LTE/5G Connectivity Module**
|
||||
|
||||
- Пропускна здатність до 600 Мбіт/с
|
||||
- 5G sub-6 і mmWave, SA і NSA операції
|
||||
- 4G Cat 20, до 7xCA, 256-QAM DL/UL, 2xCA UL
|
||||
@@ -143,7 +139,6 @@ AIRLink Enterprise ідеально підходить для швидкого
|
||||

|
||||
|
||||
- **Left side interfaces:**
|
||||
|
||||
- Power input with voltage & current monitoring
|
||||
- Місійний комп'ютер зі ШІ з картою пам'яті micro SD
|
||||
- Карта micro SD для польотного контролера
|
||||
@@ -171,13 +166,13 @@ AIRLink Enterprise ідеально підходить для швидкого
|
||||
|
||||
- **RC Connector - JST GH SM06B-GHS-TB**
|
||||
|
||||
| Номер виводу | Назва виводу | Напрямок | Напруга | Функція | | | |
|
||||
| ------------ | ----------------------------- | -------- | --------------------- | ----------------- | - | --- | ------ |
|
||||
| 1 | 5V | OUT | +5V | Вихід 5В | | | |
|
||||
| 2 | PPM_IN | IN | +3.3V | PPM вхід | | | |
|
||||
| 3 | RSSI_IN | IN | +3.3V | RSSI вхід | | | |
|
||||
| 4 | FAN_OUT | OUT | +5V | Вихід вентилятора | | | |
|
||||
| 5 | SBUS_OUT | OUT | +3.3V | SBUS output | 6 | GND | Ground |
|
||||
\| Pin number | Pin name | Direction | Voltage | Function |
|
||||
\| ---------- | -------- | --------- | ------- | ----------- | --- | --- | ------ |
|
||||
\| 1 | 5V | OUT | +5V | 5V output |
|
||||
\| 2 | PPM_IN | IN | +3.3V | PPM input |
|
||||
\| 3 | RSSI_IN | IN | +3.3V | RSSI input |
|
||||
\| 4 | FAN_OUT | OUT | +5V | Fan output |
|
||||
\| 5 | SBUS_OUT | OUT | +3.3V | SBUS output | 6 | GND | Ground |
|
||||
|
||||
* **FMU SD card - microSD**
|
||||
|
||||
@@ -186,7 +181,6 @@ AIRLink Enterprise ідеально підходить для швидкого
|
||||

|
||||
|
||||
- **Right side interfaces:**
|
||||
|
||||
- Ethernet-порт з виходом живлення
|
||||
- Телеметричний порт
|
||||
- Другий GPS-порт
|
||||
@@ -252,7 +246,6 @@ AIRLink Enterprise ідеально підходить для швидкого
|
||||

|
||||
|
||||
- **Front side interfaces:**
|
||||
|
||||
- Основний порт GNSS і компаса
|
||||
- Основний телеметричний порт
|
||||
- Вхід для камери CSI
|
||||
@@ -310,7 +303,6 @@ AIRLink Enterprise ідеально підходить для швидкого
|
||||

|
||||
|
||||
- **Rear side interfaces:**
|
||||
|
||||
- Вхід SBUS
|
||||
- 16 вихідних каналів ШІМ
|
||||
- 2 гнізда для антен LTE (MIMO)
|
||||
|
||||
@@ -25,6 +25,7 @@ This category includes boards that are not fully compliant with the pixhawk stan
|
||||
- [CubePilot Cube Orange+](../flight_controller/cubepilot_cube_orangeplus.md)
|
||||
- [CubePilot Cube Orange](../flight_controller/cubepilot_cube_orange.md)
|
||||
- [CubePilot Cube Yellow](../flight_controller/cubepilot_cube_yellow.md)
|
||||
- [Gear Up AirBrainH743](../flight_controller/gearup_airbrainh743.md)
|
||||
- [Holybro Kakute H7v2](../flight_controller/kakuteh7v2.md)
|
||||
- [Holybro Kakute H7mini](../flight_controller/kakuteh7mini.md)
|
||||
- [Holybro Kakute H7](../flight_controller/kakuteh7.md)
|
||||
|
||||
@@ -0,0 +1,96 @@
|
||||
# Gear Up AirBrainH743
|
||||
|
||||
:::warning
|
||||
PX4 не розробляє цей (або будь-який інший) автопілот.
|
||||
Contact the [manufacturer](https://takeyourgear.com/) for hardware support.
|
||||
:::
|
||||
|
||||
:::info
|
||||
This flight controller is [manufacturer supported](../flight_controller/autopilot_manufacturer_supported.md).
|
||||
:::
|
||||
|
||||
Purchase from [takeyourgear.com](https://takeyourgear.com/pages/products/airbrain).
|
||||
|
||||
For more information and pinout, check the [GitHub documentation](https://github.com/GearUp-Company/AirBrainH743).
|
||||
|
||||
## Основні характеристики
|
||||
|
||||
- MCU: Процесор STM32H743 32-біт, який працює на частоті 480 МГц
|
||||
- IMU: ICM42688P
|
||||
- Barometer: DPS310
|
||||
- Magnetometer: LIS2MDL (internal)
|
||||
- 128MB NAND Flash for logging (W25N)
|
||||
- 7x UARTs
|
||||
- I2C, SPI
|
||||
- 9x PWM Outputs (8 Motor outputs, 1 LED strip)
|
||||
- Battery input voltage: 3S-10S
|
||||
- Battery voltage/current monitoring
|
||||
- 5V@2A and 10V@2.5A BEC outputs
|
||||
- USB Type-C (IP68)
|
||||
- EMC and ESD protection
|
||||
|
||||
## Конектори та контакти
|
||||
|
||||
:::warning
|
||||
The pin order is different from the Pixhawk standard (compatible to the Betaflight standard).
|
||||
:::
|
||||
|
||||
### UARTs
|
||||
|
||||
Current UART configuration:
|
||||
|
||||
| UART | Пристрій | Функція |
|
||||
| ------ | ---------- | --------------------------------------- |
|
||||
| USART1 | /dev/ttyS0 | Console/Debug |
|
||||
| USART2 | /dev/ttyS1 | RC-вхід |
|
||||
| USART3 | /dev/ttyS2 | TEL4 (DJI/MSP) |
|
||||
| UART4 | /dev/ttyS3 | TEL1 |
|
||||
| UART5 | /dev/ttyS4 | TEL2 |
|
||||
| UART7 | /dev/ttyS5 | TEL3 (ESC Telemetry) |
|
||||
| UART8 | /dev/ttyS6 | GPS1 |
|
||||
|
||||
### Motor/Servo Outputs
|
||||
|
||||
| З’єднання | Pin | Функція |
|
||||
| --------- | --- | ---------------------------- |
|
||||
| ESC | M1 | Двигун 1 |
|
||||
| ESC | M2 | Motor 2 |
|
||||
| ESC | M3 | Motor 3 |
|
||||
| ESC | M4 | Motor 4 |
|
||||
| PWM | M5 | Motor 5 |
|
||||
| PWM | M6 | Motor 6 |
|
||||
| PWM | M7 | Motor 7 |
|
||||
| PWM | M8 | Motor 8 |
|
||||
| AUX | M9 | LED/PWM/etc. |
|
||||
|
||||
<a id="bootloader"></a>
|
||||
|
||||
## Оновлення завантажувача PX4
|
||||
|
||||
Before PX4 firmware can be installed, the _PX4 bootloader_ must be flashed.
|
||||
Download the [gearup_airbrainh743_bootloader.bin](https://github.com/PX4/PX4-Autopilot/blob/main/boards/gearup/airbrainh743/extras/gearup_airbrainh743_bootloader.bin) bootloader binary and read [this page](../advanced_config/bootloader_update_from_betaflight.md) for flashing instructions.
|
||||
|
||||
## Збірка прошивки
|
||||
|
||||
To [build PX4](../dev_setup/building_px4.md) for this target:
|
||||
|
||||
```
|
||||
make gearup_airbrainh743_default
|
||||
```
|
||||
|
||||
## Встановлення прошивки PX4
|
||||
|
||||
Firmware can be installed in any of the normal ways:
|
||||
|
||||
- Збудуйте та завантажте джерело:
|
||||
|
||||
```
|
||||
make gearup_airbrainh743_default upload
|
||||
```
|
||||
|
||||
- [Load the firmware](../config/firmware.md) using _QGroundControl_.
|
||||
Ви можете використовувати або готове вбудоване програмне забезпечення, або власне користувацьке програмне забезпечення.
|
||||
|
||||
### Системна консоль
|
||||
|
||||
UART1 (ttyS0) is configured for use as the [System Console](../debug/system_console.md).
|
||||
@@ -231,7 +231,7 @@ Ackermann rovers do not support the yaw setpoint.
|
||||
|
||||
- Position setpoint **and** velocity setpoint (the velocity setpoint is used as feedforward; it is added to the output of the position controller and the result is used as the input to the velocity controller).
|
||||
|
||||
- PX4 supports the following `coordinate_frame` values (only): [MAV_FRAME_GLOBAL](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL).
|
||||
- PX4 supports the following `coordinate_frame` values (only): [MAV_FRAME_GLOBAL_INT](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL_INT), [MAV_FRAME_GLOBAL_RELATIVE_ALT_INT](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL_RELATIVE_ALT_INT), [MAV_FRAME_GLOBAL_TERRAIN_ALT_INT](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL_TERRAIN_ALT_INT).
|
||||
|
||||
- [SET_ATTITUDE_TARGET](https://mavlink.io/en/messages/common.html#SET_ATTITUDE_TARGET)
|
||||
- Підтримуються наступні вхідні комбінації:
|
||||
@@ -277,7 +277,7 @@ Ackermann rovers do not support the yaw setpoint.
|
||||
- 12288: Задання Loiter (політ по колу, центрованому на заданій точці).
|
||||
- 16384: Задання бездіяльності (нульовий газ, нульовий крен/тангаж).
|
||||
|
||||
- PX4 supports the following `coordinate_frame` values (only): [MAV_FRAME_GLOBAL](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL).
|
||||
- PX4 supports the following `coordinate_frame` values (only): [MAV_FRAME_GLOBAL_INT](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL_INT), [MAV_FRAME_GLOBAL_RELATIVE_ALT_INT](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL_RELATIVE_ALT_INT), [MAV_FRAME_GLOBAL_TERRAIN_ALT_INT](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL_TERRAIN_ALT_INT).
|
||||
|
||||
- [SET_ATTITUDE_TARGET](https://mavlink.io/en/messages/common.html#SET_ATTITUDE_TARGET)
|
||||
- Підтримуються наступні вхідні комбінації:
|
||||
@@ -286,7 +286,29 @@ Ackermann rovers do not support the yaw setpoint.
|
||||
|
||||
### Ровер
|
||||
|
||||
Rover does not support a MAVLink offboard API (ROS2 is supported).
|
||||
Rover supports offboard control using the generic MAVLink position/velocity setpoint messages listed below.
|
||||
These are converted into a [TrajectorySetpoint](../msg_docs/TrajectorySetpoint.md) internally, and then into rover setpoints by the rover offboard modes.
|
||||
For rover-specific control setpoints and better behaviour we recommend using the [Rover Setpoints](#rover-setpoints) via ROS 2.
|
||||
|
||||
:::info
|
||||
Rover MAVLink setpoints are gated by the MAVLink parameter [MAV_FWDEXTSP](../advanced_config/parameter_reference.md#MAV_FWDEXTSP) (Forward external setpoint messages).
|
||||
:::
|
||||
|
||||
- [SET_POSITION_TARGET_LOCAL_NED](https://mavlink.io/en/messages/common.html#SET_POSITION_TARGET_LOCAL_NED)
|
||||
- Position setpoint: `x`, `y` in [MAV_FRAME_LOCAL_NED](https://mavlink.io/en/messages/common.html#MAV_FRAME_LOCAL_NED) (`z` is ignored by rover modules).
|
||||
- Velocity setpoint: `vx`, `vy` in [MAV_FRAME_LOCAL_NED](https://mavlink.io/en/messages/common.html#MAV_FRAME_LOCAL_NED) or [MAV_FRAME_BODY_NED](https://mavlink.io/en/messages/common.html#MAV_FRAME_BODY_NED).
|
||||
- `yaw`/`yaw_rate`:
|
||||
- Ackermann/Differential: ignored (in velocity control the yaw setpoint is derived from the velocity direction).
|
||||
- Mecanum: can be controlled independently (decoupled) using `yaw`/`yaw_rate`.
|
||||
- Acceleration setpoints (`afx`, `afy`, `afz`) are ignored by rover modules.
|
||||
|
||||
- [SET_POSITION_TARGET_GLOBAL_INT](https://mavlink.io/en/messages/common.html#SET_POSITION_TARGET_GLOBAL_INT)
|
||||
- Position setpoint: `lat_int`, `lon_int`, `alt` (converted into local NED internally; rover modules only use the horizontal components).
|
||||
- Velocity setpoint: `vx`, `vy`, `vz` (rover modules use only the horizontal components).
|
||||
- PX4 supports the following `coordinate_frame` values (only): [MAV_FRAME_GLOBAL_INT](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL_INT), [MAV_FRAME_GLOBAL_RELATIVE_ALT_INT](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL_RELATIVE_ALT_INT), [MAV_FRAME_GLOBAL_TERRAIN_ALT_INT](https://mavlink.io/en/messages/common.html#MAV_FRAME_GLOBAL_TERRAIN_ALT_INT).
|
||||
|
||||
- [SET_ATTITUDE_TARGET](https://mavlink.io/en/messages/common.html#SET_ATTITUDE_TARGET)
|
||||
- Not supported for rover offboard control.
|
||||
|
||||
## Параметри для відключення
|
||||
|
||||
|
||||
@@ -28,7 +28,6 @@ _Режим місії_ змушує транспортний засіб вик
|
||||
На високому рівні всі типи транспортних засобів ведуть себе однаково, коли ввімкнено режим МІСІЯ:
|
||||
|
||||
1. Якщо місія не збережена, або якщо PX4 завершив виконання всіх команд місії, або якщо [місія не є можливою](#mission-feasibility-checks):
|
||||
|
||||
- Якщо літає транспортний засіб, він буде марнувати час.
|
||||
- Якщо посадять транспортний засіб, він буде "чекати".
|
||||
|
||||
|
||||
@@ -115,7 +115,6 @@ The altitude control mode determine whether the vehicle altitude is relative to
|
||||
Відносна відстань до дрона до цілі зміниться, коли ви підніметесь та опуститесь (використовуйте обережно в гірській місцевості).
|
||||
|
||||
- `2D + Terrain` makes the drone follow at a fixed height relative to the terrain underneath it, using information from a distance sensor.
|
||||
|
||||
- If the vehicle does not have a distance sensor following will be identical to `2D tracking`.
|
||||
- Датчики відстані не завжди точні, і транспортні засоби можуть бути "скачущими" під час польоту в цьому режимі.
|
||||
- Зверніть увагу, що висота вимірюється відносно землі під транспортним засобом, а не цільового об'єкта.
|
||||
|
||||
@@ -30,7 +30,6 @@ They may also be created by a MAVLink API such as [MAVSDK](../robotics/mavsdk.md
|
||||
На високому рівні всі типи транспортних засобів ведуть себе однаково, коли ввімкнено режим МІСІЯ:
|
||||
|
||||
1. Якщо місія не збережена, або якщо PX4 завершив виконання всіх команд місії, або якщо [місія не є можливою](#mission-feasibility-checks):
|
||||
|
||||
- Якщо літає транспортний засіб, він буде утримувати.
|
||||
- Якщо посадять транспортний засіб, він буде "чекати".
|
||||
|
||||
|
||||
@@ -49,7 +49,6 @@ VTOL підтримує [інші типи повернення PX4](../flight_m
|
||||
Місійний маршрут посадки для літального апарату типу VTOL складається з [MAV_CMD_DO_LAND_START](https://mavlink.io/en/messages/common.html#MAV_CMD_DO_LAND_START), однієї або кількох маршрутних точок розташування та [MAV_CMD_NAV_VTOL_LAND](https://mavlink.io/en/messages/common.html#MAV_CMD_NAV_VTOL_LAND).
|
||||
|
||||
- Якщо призначенням є точка збору або домашня локація, апарат:
|
||||
|
||||
- Переводиться в режим ожидання/спірального спуску на висоту [RTL_DESCEND_ALT](#RTL_DESCEND_ALT).
|
||||
- Кружляє протягом короткого часу, визначеного [RTL_LAND_DELAY](#RTL_LAND_DELAY).
|
||||
- Повертається по напрямку до призначення (центр кругового руху).
|
||||
|
||||
@@ -30,7 +30,7 @@ The diagrams use the standard [PX4 notation](../contribute/notation.md) (and eac
|
||||
|
||||
::: info
|
||||
The IMU pipeline is:
|
||||
gyro data > apply calibration parameters > remove estimated bias > notch filter (`IMU_GYRO_NF0_BW` and `IMU_GYRO_NF0_FRQ`) > low-pass filter (`IMU_GYRO_CUTOFF`) > vehicle_angular_velocity (_filtered angular rate used by the P and I controllers_) > derivative -> low-pass filter (`IMU_DGYRO_CUTOFF`) > vehicle_angular_acceleration (_filtered angular acceleration used by the D controller_)
|
||||
gyro data > apply calibration parameters > remove estimated bias > notch filter (`IMU_GYRO_NF0_BW` and `IMU_GYRO_NF0_FRQ`) > low-pass filter (`IMU_GYRO_CUTOFF`) > vehicle_angular_velocity (\_filtered angular rate used by the P and I controllers_) > derivative -> low-pass filter (`IMU_DGYRO_CUTOFF`) > vehicle_angular_acceleration (\_filtered angular acceleration used by the D controller_)
|
||||
|
||||

|
||||
|
||||
@@ -177,7 +177,7 @@ The angular position of the control effectors (ailerons, elevators, rudders, ...
|
||||
Крім того, оскільки керуючі поверхні ефективніші при високій швидкості і менш ефективні при низькій швидкості, контролер, налаштований на крейсерську швидкість, масштабується за допомогою вимірів швидкості повітря (якщо використовується такий датчик).
|
||||
|
||||
:::info
|
||||
If no airspeed sensor is used then gain scheduling for the FW attitude controller is disabled (it's open loop); no correction is/can be made in TECS using airspeed feedback.
|
||||
If no airspeed sensor is used then gain scheduling for the FW attitude controller is disabled (it's open loop); no correction is/can be made in TECS using airspeed feedback.
|
||||
:::
|
||||
|
||||
The feedforward gain is used to compensate for aerodynamic damping.
|
||||
@@ -187,7 +187,7 @@ The feedforward gain is used to compensate for aerodynamic damping.
|
||||
### Поворотна координація
|
||||
|
||||
Контролери крену та тангажу мають однакову структуру, і довжинна та поперечна динаміка вважаються достатньо роз'єднаними, щоб працювати незалежно один від одного.
|
||||
Контролер курсу, однак, генерує встановлення швидкості курсу, використовуючи обмеження координації повороту для мінімізації бокового прискорення, що виникає, коли літак слідкує. Алгоритм узгодження повороту базується виключно на узгодженому розрахунку геометрії повороту.
|
||||
Контролер курсу, однак, генерує встановлення швидкості курсу, використовуючи обмеження координації повороту для мінімізації бокового прискорення, що виникає, коли літак слідкує. Алгоритм узгодження повороту базується виключно на узгодженому розрахунку геометрії повороту.
|
||||
|
||||
$$\dot{\Psi}_{sp} = \frac{g}{V_T} \tan{\phi_{sp}} \cos{\theta_{sp}}$$
|
||||
|
||||
|
||||
@@ -33,7 +33,6 @@ Note that if landed, the next mission item after deployment should be another `W
|
||||
1. Create a normal mission with a `Takeoff` mission item, and additional waypoints for your required flight path.
|
||||
|
||||
2. Додайте маршрутну точку на карті, де ви хочете випустити посилку.
|
||||
|
||||
- Щоб скинути посилку під час польоту, установіть відповідну висоту для маршрутної точки (і переконайтеся, що маршрутна точка знаходиться в безпечному місці для скидання посилки).
|
||||
|
||||
- If you'd like to land the vehicle to make the delivery you will need to change the `Waypoint` to a `Land` mission item.
|
||||
|
||||
@@ -7,6 +7,12 @@ Support for rover is [experimental](../airframes/index.md#experimental-vehicles)
|
||||
Maintainer volunteers, [contribution](../contribute/index.md) of new features, new frame configurations, or other improvements would all be very welcome!
|
||||
:::
|
||||
|
||||
:::tip
|
||||
Rover is not in the default PX4 firmware downloaded from QGC.
|
||||
Unlike for other vehicle types you will need to install it as custom firmware.
|
||||
For more information see [Flashing the Rover Build](../config_rover/index.md#flashing-the-rover-build).
|
||||
:::
|
||||
|
||||

|
||||
|
||||
PX4 provides support for the three most common types of rovers:
|
||||
|
||||
@@ -20,7 +20,7 @@ It is possible to have a GPS lock (Green LED) and still not be able to arm the v
|
||||
:::
|
||||
|
||||
:::tip
|
||||
In the event of an error (blinking red), or if the vehicle can't achieve GPS lock (change from blue to green), check for more detailed status information in _QGroundControl_ including calibration status, and errors messages reported by the [Preflight Checks (Internal)](../flying/pre_flight_checks.md).
|
||||
In the event of an error (blinking red), or if the vehicle can't achieve GPS lock (change from blue to green), check for more detailed status information in _QGroundControl_ including calibration status, and errors messages reported by the [Preflight Checks (Internal)](../flying/pre_flight_checks.md).
|
||||
Також перевірте, чи правильно підключений GPS-модуль, чи правильно Pixhawk зчитує ваш GPS, і чи правильно GPS передає дані про місцеперебування.
|
||||
:::
|
||||
|
||||
@@ -47,7 +47,8 @@ In the event of an error (blinking red), or if the vehicle can't achieve GPS loc
|
||||
Під час аварійного режиму апарат намагатиметься повернутися до місця зльоту або може просто знизитися там, де він зараз перебуває.
|
||||
|
||||
- **[Solid Amber] Low Battery Warning:** Indicates your vehicle's battery is running dangerously low.
|
||||
Після певного моменту пристрій перейде у failsafe режим. Однак цей режим повинен сигналізувати про те, що настав час завершити політ.
|
||||
Після певного моменту пристрій перейде у failsafe режим. However, this mode should signal caution that it's time to end
|
||||
this flight.
|
||||
|
||||
- **[Blinking Red] Error / Setup Required:** Indicates that your autopilot needs to be configured or calibrated before flying.
|
||||
Під'єднайте автопілот до наземної станції керування, щоб перевірити, в чому проблема.
|
||||
@@ -77,11 +78,11 @@ The LED labels shown above are commonly used, but might differ on some boards.
|
||||
|
||||
Більш детальна інформація про те, як інтерпретувати світлодіодні індикатори, наведені нижче (де "х" означає "будь-який стан")
|
||||
|
||||
| Червоний/помаранчевий | Синій | Зелений | Значення |
|
||||
| --------------------- | ----- | ------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
|
||||
| 10 Гц | x | x | Overload CPU load > 80%, or RAM usage > 98% |
|
||||
| ВИМК | x | x | Overload CPU load <= 80%, or RAM usage <= 98% |
|
||||
| NA | ВИМК | 4 Гц | actuator_armed->armed && failsafe |
|
||||
| NA | УВІМК | 4 Гц | actuator_armed->armed && !failsafe |
|
||||
| NA | ВИМК | 1 Гц | !actuator_armed-> armed && actuator_armed->ready_to_arm |
|
||||
| NA | ВИМК | 10 Гц | !actuator_armed->armed && !actuator_armed->ready_to_arm |
|
||||
| Червоний/помаранчевий | Синій | Зелений | Значення |
|
||||
| --------------------- | ----- | ------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| 10 Гц | x | x | Overload CPU load > 80%, or RAM usage > 98% |
|
||||
| ВИМК | x | x | Overload CPU load <= 80%, or RAM usage <= 98% |
|
||||
| NA | ВИМК | 4 Гц | actuator_armed->armed && failsafe |
|
||||
| NA | УВІМК | 4 Гц | actuator_armed->armed && !failsafe |
|
||||
| NA | ВИМК | 1 Гц | !actuator_armed-> armed && actuator_armed->ready_to_arm |
|
||||
| NA | ВИМК | 10 Гц | !actuator_armed->armed && !actuator_armed->ready_to_arm |
|
||||
|
||||
@@ -13,7 +13,7 @@ You can search for tune use using the string `TUNE_ID_name`(e.g. \`TUNE_ID_PARAC
|
||||
|
||||
Ці мелодії відтворюються під час завантаження.
|
||||
|
||||
<!-- https://github.com/PX4/PX4-Autopilot/blob/main/ROMFS/px4fmu_common/init.d/rcS -->
|
||||
<!-- https://github.com/PX4/PX4-Autopilot/blob/main/ROMFS/px4fmu_common/init.d/rcS -->
|
||||
|
||||
#### Сигнал запуску
|
||||
|
||||
|
||||
@@ -152,7 +152,6 @@ This should be set by default, but if not, follow the [MAVLink2 configuration in
|
||||

|
||||
|
||||
4. Після завершення опитування:
|
||||
|
||||
- The RTK GPS icon changes to white and _QGroundControl_ starts to stream position data to the vehicle:
|
||||
|
||||

|
||||
|
||||
+21
-69
@@ -3,19 +3,11 @@ import { useData } from 'vitepress'
|
||||
const { site } = useData();
|
||||
</script>
|
||||
|
||||
<div style="float:right; padding:10px; margin-right:20px;"><a href="https://px4.io/"><img src="../assets/site/logo_pro_small.png" title="PX4 Logo" width="180px" /></a></div>
|
||||
|
||||
# Посібник користувача автопілота PX4
|
||||
|
||||
[](https://github.com/PX4/PX4-Autopilot/releases) [](https://discuss.px4.io//) [](https://discord.gg/dronecode)
|
||||
|
||||
PX4 is the _Professional Autopilot_.
|
||||
Розроблений розробниками світового класу з дрон індустрії та наукових закладів і активно підтримується спільнотою у світі. Він дозволяє працювати з різними типами безпілотних транспортних засобів від гоночних, вантажних дронів до сухопутних автомобілів та надводних човнів.
|
||||
|
||||
:::tip
|
||||
This guide contains everything you need to assemble, configure, and safely fly a PX4-based vehicle.
|
||||
Хочете зробити внесок? Check out the [Development](development/development.md) section.
|
||||
:::
|
||||
PX4 is an open-source autopilot for drones and autonomous vehicles. It runs on multirotors, fixed-wing, VTOL, helicopters, rovers, and more. This guide covers everything from assembly and configuration to flight operations and development.
|
||||
|
||||
<div v-if="site.title == 'PX4 Guide (main)'">
|
||||
|
||||
@@ -29,83 +21,43 @@ Documented changes since the stable release are captured in the evolving [releas
|
||||
|
||||
</div>
|
||||
|
||||
## Як почати?
|
||||
## For Developers
|
||||
|
||||
[Basic Concepts](getting_started/px4_basic_concepts.md) should be read by all users!
|
||||
It provides an overview of PX4, including features provided by the flight stack (flight modes and safety features) and the supported hardware (flight controller, vehicle types, telemetry systems, RC control systems).
|
||||
:::tip
|
||||
Building on PX4 or extending the platform? Start here: [Development Guide](development/development.md). Set up your [dev environment](dev_setup/config_initial.md), [build from source](dev_setup/building_px4.md), run [SITL simulation](simulation/index.md), or integrate via [ROS 2](ros2/index.md) and [MAVSDK](https://mavsdk.mavlink.io/).
|
||||
:::
|
||||
|
||||
Залежно від того, чого ви хочете досягти, наступні поради допоможуть вам мандрувати по цьому посібнику:
|
||||
## Початок роботи
|
||||
|
||||
### I want a vehicle that works with PX4
|
||||
Start with [Basic Concepts](getting_started/px4_basic_concepts.md) for an overview of the flight stack, flight modes, safety features, and supported hardware.
|
||||
|
||||
In the [Multicopter](frames_multicopter/index.md), [VTOL](frames_vtol/index.md), and [Plane (Fixed-Wing)](frames_plane/index.md) sections you'll find topics like the following (these links are for multicopter):
|
||||
## Build a Vehicle
|
||||
|
||||
- [Complete Vehicles](complete_vehicles_mc/index.md) list "Ready to Fly" (RTF) pre-built vehicles
|
||||
- [Kits](frames_multicopter/kits.md) lists drones that you have to build yourself from a set of preselected parts
|
||||
- [DIY Builds](frames_multicopter/diy_builds.md) shows some examples of drones that have been built using parts that were sourced individually
|
||||
Pick your frame type: [Multicopter](frames_multicopter/index.md), [Fixed-Wing](frames_plane/index.md), [VTOL](frames_vtol/index.md), [Helicopter](frames_helicopter/index.md), or [Rover](frames_rover/index.md). Each section covers complete vehicles, kits, and DIY builds. For assembly instructions see [Assembling a Multicopter](assembly/assembly_mc.md) or the equivalent for your frame.
|
||||
|
||||
Both kits and complete vehicles usually include everything you need except for a battery and RC System.
|
||||
Kits are usually not hard to build, provide a good introduction to how drones fit together, and are relatively inexpensive.
|
||||
We provide generic instructions for assembly, such as [Assembling a Multicopter](assembly/assembly_mc.md), and most kits come with specific instructions too.
|
||||
## Configure and Tune
|
||||
|
||||
If the kits and complete drones aren't quite right for you then you can build a vehicle from scratch, but this requires more knowledge.
|
||||
[Airframe Builds](airframes/index.md) lists the supported frame starting points to give you some idea of what is possible.
|
||||
Once assembled, follow the configuration guide for your vehicle type (e.g. [Multicopter Configuration](config_mc/index.md)). This covers sensor calibration, flight mode setup, and tuning.
|
||||
|
||||
Once you have a vehicle that supports PX4 you will need to configure it and calibrate the sensors.
|
||||
Each vehicle type has its own configuration section that explains the main steps, such as [Multicopter Configuration/Tuning](config_mc/index.md).
|
||||
## Апаратне забезпечення(Hardware)
|
||||
|
||||
### I want to add a payload/camera
|
||||
The [Hardware Selection & Setup](hardware/drone_parts.md) section covers flight controllers, sensors, telemetry, RC systems, and payloads. See [Payloads](payloads/index.md) for camera and delivery integrations.
|
||||
|
||||
The [Payloads](payloads/index.md) section describes how to add a camera and how to configure PX4 to enable you to deliver packages.
|
||||
## Fly
|
||||
|
||||
### I am modifying a supported vehicle
|
||||
Read [Operations](config/operations.md) to understand safety features and failsafe behavior before your first flight. Then see [Basic Flying (Multicopter)](flying/basic_flying_mc.md) or the equivalent for your frame type.
|
||||
|
||||
The [Hardware Selection & Setup](hardware/drone_parts.md) section provides both high level and product-specific information about hardware that you might use with PX4 and its configuration.
|
||||
This is the first place you should look if you want to modify a drone and add new components.
|
||||
## Підтримка
|
||||
|
||||
### I want to fly
|
||||
|
||||
Before you fly you should read [Operations](config/operations.md) to understand how to set up the safety features of your vehicle and the common behaviours of all frame types.
|
||||
Once you've done that you're ready to fly.
|
||||
|
||||
Basic instructions for flying each vehicle type are provided in the respective sections, such as [Basic Flying (Multicopter)](flying/basic_flying_mc.md).
|
||||
|
||||
### I want to run PX4 on a new Flight Controller and extend the platform
|
||||
|
||||
The [Development](development/development.md) section explains how to support new airframes and types of vehicles, modify flight algorithms, add new modes, integrate new hardware, communicate with PX4 from outside the flight controller, and contribute to PX4.
|
||||
|
||||
## Отримання допомоги
|
||||
|
||||
The [Support](contribute/support.md) page explains how to get help from the core dev team and the wider community.
|
||||
|
||||
Серед інших речей, які вона покриває:
|
||||
|
||||
- [Forums where you can get help](contribute/support.md#forums-and-chat)
|
||||
- [Diagnosing issues](contribute/support.md#diagnosing-problems)
|
||||
- [How to report bugs](contribute/support.md#issue-bug-reporting)
|
||||
- [Weekly dev call](contribute/support.md#weekly-dev-call)
|
||||
|
||||
## Reporting Bugs & Issues
|
||||
|
||||
If you have any problems using PX4 first post them on the [support forums](contribute/support.md#forums-and-chat) (as they may be caused by vehicle configuration).
|
||||
|
||||
If directed by the development team, code issues may be raised on [Github here](https://github.com/PX4/PX4-Autopilot/issues).
|
||||
Where possible provide [flight logs](getting_started/flight_reporting.md) and other information requested in the issue template.
|
||||
Get help on the [discussion forums](https://discuss.px4.io/) or [Discord](https://discord.gg/dronecode). See the [Support](contribute/support.md) page for diagnosing problems, reporting bugs, and joining the [weekly dev call](contribute/dev_call.md).
|
||||
|
||||
## Долучитись до проєкту
|
||||
|
||||
Information on how to contribute to code and documentation can be found in the [Contributing](contribute/index.md) section:
|
||||
|
||||
- [Code](contribute/index.md)
|
||||
- [Documentation](contribute/docs.md)
|
||||
- [Translation](contribute/translation.md)
|
||||
See the [Contributing](contribute/index.md) section for code, [documentation](contribute/docs.md), and [translation](contribute/translation.md) guidelines.
|
||||
|
||||
## Переклади
|
||||
|
||||
There are several [translations](contribute/translation.md) of this guide.
|
||||
Ви можете отримати доступ до вибору конкретного доступного переклада з меню Мови (вгорі праворуч):
|
||||
|
||||

|
||||
There are several [translations](contribute/translation.md) of this guide. Use the language selector in the top navigation.
|
||||
|
||||
<!--@include: _contributors.md-->
|
||||
|
||||
@@ -141,9 +93,9 @@ The calendar default timezone is Central European Time (CET).
|
||||
|
||||
## Управління
|
||||
|
||||
The PX4 flight stack is hosted under the governance of the [Dronecode Project](https://dronecode.org/).
|
||||
The PX4 Autopilot project is hosted by the [Dronecode Foundation](https://www.dronecode.org/), a [Linux Foundation](https://www.linuxfoundation.org/) Collaborative Project. Dronecode holds all PX4 trademarks and serves as the project's legal guardian, ensuring vendor-neutral stewardship. No single company owns the name or controls the roadmap. The source code is licensed under the [BSD 3-Clause](https://opensource.org/license/BSD-3-Clause) license, so you are free to use, modify, and distribute it in your own projects.
|
||||
|
||||
<a href="https://dronecode.org/" style="padding:20px" ><img src="../assets/site/logo_dronecode.png" alt="Dronecode Logo" width="110px"/></a> <a href="https://www.linuxfoundation.org/projects" style="padding:20px;"><img src="../assets/site/logo_linux_foundation.png" alt="Linux Foundation Logo" width="80px" /></a>
|
||||
<a href="https://www.dronecode.org/" style="padding:20px"><img src="../assets/site/dronecode_logo.svg" alt="Dronecode Logo" width="140px"/></a> <a href="https://www.linuxfoundation.org/projects" style="padding:20px;"><img src="../assets/site/logo_linux_foundation.png" alt="Linux Foundation Logo" width="80px" /></a>
|
||||
|
||||
<div style="padding:10px"> </div>
|
||||
|
||||
|
||||
+191
-183
@@ -95,192 +95,200 @@ They are not build into the module, and hence are neither published or subscribe
|
||||
:::details
|
||||
See messages
|
||||
|
||||
- [BatteryInfo](../msg_docs/BatteryInfo.md)
|
||||
- [TakeoffStatus](../msg_docs/TakeoffStatus.md)
|
||||
- [SensorGnssStatus](../msg_docs/SensorGnssStatus.md)
|
||||
- [Airspeed](../msg_docs/Airspeed.md)
|
||||
- [PpsCapture](../msg_docs/PpsCapture.md)
|
||||
- [ActuatorControlsStatus](../msg_docs/ActuatorControlsStatus.md)
|
||||
- [CameraCapture](../msg_docs/CameraCapture.md)
|
||||
- [Px4ioStatus](../msg_docs/Px4ioStatus.md)
|
||||
- [FuelTankStatus](../msg_docs/FuelTankStatus.md)
|
||||
- [VehicleAngularVelocity](../msg_docs/VehicleAngularVelocity.md)
|
||||
- [VehicleOpticalFlow](../msg_docs/VehicleOpticalFlow.md)
|
||||
- [AirspeedWind](../msg_docs/AirspeedWind.md)
|
||||
- [OrbTest](../msg_docs/OrbTest.md)
|
||||
- [GimbalDeviceInformation](../msg_docs/GimbalDeviceInformation.md)
|
||||
- [GpioOut](../msg_docs/GpioOut.md)
|
||||
- [PurePursuitStatus](../msg_docs/PurePursuitStatus.md)
|
||||
- [Gripper](../msg_docs/Gripper.md)
|
||||
- [VehicleAirData](../msg_docs/VehicleAirData.md)
|
||||
- [TuneControl](../msg_docs/TuneControl.md)
|
||||
- [DebugVect](../msg_docs/DebugVect.md)
|
||||
- [HoverThrustEstimate](../msg_docs/HoverThrustEstimate.md)
|
||||
- [HomePositionV0](../msg_docs/HomePositionV0.md)
|
||||
- [SensorsStatusImu](../msg_docs/SensorsStatusImu.md)
|
||||
- [EstimatorAidSource3d](../msg_docs/EstimatorAidSource3d.md)
|
||||
- [EstimatorBias](../msg_docs/EstimatorBias.md)
|
||||
- [GpioConfig](../msg_docs/GpioConfig.md)
|
||||
- [SystemPower](../msg_docs/SystemPower.md)
|
||||
- [RateCtrlStatus](../msg_docs/RateCtrlStatus.md)
|
||||
- [MissionResult](../msg_docs/MissionResult.md)
|
||||
- [PowerButtonState](../msg_docs/PowerButtonState.md)
|
||||
- [EscStatus](../msg_docs/EscStatus.md)
|
||||
- [HealthReport](../msg_docs/HealthReport.md)
|
||||
- [VehicleMagnetometer](../msg_docs/VehicleMagnetometer.md)
|
||||
- [SensorGyro](../msg_docs/SensorGyro.md)
|
||||
- [GpioRequest](../msg_docs/GpioRequest.md)
|
||||
- [DebugKeyValue](../msg_docs/DebugKeyValue.md)
|
||||
- [DistanceSensorModeChangeRequest](../msg_docs/DistanceSensorModeChangeRequest.md)
|
||||
- [ParameterUpdate](../msg_docs/ParameterUpdate.md)
|
||||
- [SensorAirflow](../msg_docs/SensorAirflow.md)
|
||||
- [UavcanParameterValue](../msg_docs/UavcanParameterValue.md)
|
||||
- [EstimatorSensorBias](../msg_docs/EstimatorSensorBias.md)
|
||||
- [CanInterfaceStatus](../msg_docs/CanInterfaceStatus.md)
|
||||
- [GimbalDeviceSetAttitude](../msg_docs/GimbalDeviceSetAttitude.md)
|
||||
- [ActionRequest](../msg_docs/ActionRequest.md)
|
||||
- [LandingTargetInnovations](../msg_docs/LandingTargetInnovations.md)
|
||||
- [PwmInput](../msg_docs/PwmInput.md)
|
||||
- [PowerMonitor](../msg_docs/PowerMonitor.md)
|
||||
- [Mission](../msg_docs/Mission.md)
|
||||
- [ArmingCheckReplyV0](../msg_docs/ArmingCheckReplyV0.md)
|
||||
- [FigureEightStatus](../msg_docs/FigureEightStatus.md)
|
||||
- [RadioStatus](../msg_docs/RadioStatus.md)
|
||||
- [VehicleRoi](../msg_docs/VehicleRoi.md)
|
||||
- [RtlTimeEstimate](../msg_docs/RtlTimeEstimate.md)
|
||||
- [GimbalManagerStatus](../msg_docs/GimbalManagerStatus.md)
|
||||
- [EstimatorSelectorStatus](../msg_docs/EstimatorSelectorStatus.md)
|
||||
- [Rpm](../msg_docs/Rpm.md)
|
||||
- [VehicleAngularAccelerationSetpoint](../msg_docs/VehicleAngularAccelerationSetpoint.md)
|
||||
- [Ping](../msg_docs/Ping.md)
|
||||
- [QshellReq](../msg_docs/QshellReq.md)
|
||||
- [SensorMag](../msg_docs/SensorMag.md)
|
||||
- [EstimatorStates](../msg_docs/EstimatorStates.md)
|
||||
- [SensorUwb](../msg_docs/SensorUwb.md)
|
||||
- [OpenDroneIdArmStatus](../msg_docs/OpenDroneIdArmStatus.md)
|
||||
- [TiltrotorExtraControls](../msg_docs/TiltrotorExtraControls.md)
|
||||
- [ControlAllocatorStatus](../msg_docs/ControlAllocatorStatus.md)
|
||||
- [ParameterResetRequest](../msg_docs/ParameterResetRequest.md)
|
||||
- [SensorHygrometer](../msg_docs/SensorHygrometer.md)
|
||||
- [VehicleLocalPositionSetpoint](../msg_docs/VehicleLocalPositionSetpoint.md)
|
||||
- [AdcReport](../msg_docs/AdcReport.md)
|
||||
- [DronecanNodeStatus](../msg_docs/DronecanNodeStatus.md)
|
||||
- [EstimatorAidSource2d](../msg_docs/EstimatorAidSource2d.md)
|
||||
- [SensorAccelFifo](../msg_docs/SensorAccelFifo.md)
|
||||
- [RoverAttitudeStatus](../msg_docs/RoverAttitudeStatus.md)
|
||||
- [SensorCorrection](../msg_docs/SensorCorrection.md)
|
||||
- [UlogStream](../msg_docs/UlogStream.md)
|
||||
- [PositionControllerLandingStatus](../msg_docs/PositionControllerLandingStatus.md)
|
||||
- [GpsInjectData](../msg_docs/GpsInjectData.md)
|
||||
- [MagnetometerBiasEstimate](../msg_docs/MagnetometerBiasEstimate.md)
|
||||
- [LoggerStatus](../msg_docs/LoggerStatus.md)
|
||||
- [ParameterSetValueRequest](../msg_docs/ParameterSetValueRequest.md)
|
||||
- [SensorBaro](../msg_docs/SensorBaro.md)
|
||||
- [OrbTestMedium](../msg_docs/OrbTestMedium.md)
|
||||
- [RoverSpeedStatus](../msg_docs/RoverSpeedStatus.md)
|
||||
- [FollowTargetStatus](../msg_docs/FollowTargetStatus.md)
|
||||
- [ParameterSetUsedRequest](../msg_docs/ParameterSetUsedRequest.md)
|
||||
- [PositionControllerStatus](../msg_docs/PositionControllerStatus.md)
|
||||
- [UlogStreamAck](../msg_docs/UlogStreamAck.md)
|
||||
- [DatamanRequest](../msg_docs/DatamanRequest.md)
|
||||
- [InternalCombustionEngineControl](../msg_docs/InternalCombustionEngineControl.md)
|
||||
- [PositionSetpoint](../msg_docs/PositionSetpoint.md)
|
||||
- [DatamanResponse](../msg_docs/DatamanResponse.md)
|
||||
- [LedControl](../msg_docs/LedControl.md)
|
||||
- [MavlinkTunnel](../msg_docs/MavlinkTunnel.md)
|
||||
- [VehicleLocalPositionV0](../msg_docs/VehicleLocalPositionV0.md)
|
||||
- [Event](../msg_docs/Event.md)
|
||||
- [ActuatorArmed](../msg_docs/ActuatorArmed.md)
|
||||
- [GpioIn](../msg_docs/GpioIn.md)
|
||||
- [SensorGyroFft](../msg_docs/SensorGyroFft.md)
|
||||
- [SensorAccel](../msg_docs/SensorAccel.md)
|
||||
- [SensorsStatus](../msg_docs/SensorsStatus.md)
|
||||
- [VehicleAttitudeSetpointV0](../msg_docs/VehicleAttitudeSetpointV0.md)
|
||||
- [GeneratorStatus](../msg_docs/GeneratorStatus.md)
|
||||
- [DifferentialPressure](../msg_docs/DifferentialPressure.md)
|
||||
- [FixedWingRunwayControl](../msg_docs/FixedWingRunwayControl.md)
|
||||
- [NormalizedUnsignedSetpoint](../msg_docs/NormalizedUnsignedSetpoint.md)
|
||||
- [TrajectorySetpoint6dof](../msg_docs/TrajectorySetpoint6dof.md)
|
||||
- [LaunchDetectionStatus](../msg_docs/LaunchDetectionStatus.md)
|
||||
- [RoverRateStatus](../msg_docs/RoverRateStatus.md)
|
||||
- [AirspeedValidatedV0](../msg_docs/AirspeedValidatedV0.md)
|
||||
- [GimbalManagerSetAttitude](../msg_docs/GimbalManagerSetAttitude.md)
|
||||
- [VelocityLimits](../msg_docs/VelocityLimits.md)
|
||||
- [MagWorkerData](../msg_docs/MagWorkerData.md)
|
||||
- [Cpuload](../msg_docs/Cpuload.md)
|
||||
- [InternalCombustionEngineStatus](../msg_docs/InternalCombustionEngineStatus.md)
|
||||
- [SensorGnssRelative](../msg_docs/SensorGnssRelative.md)
|
||||
- [MavlinkLog](../msg_docs/MavlinkLog.md)
|
||||
- [SensorTemp](../msg_docs/SensorTemp.md)
|
||||
- [LandingGearWheel](../msg_docs/LandingGearWheel.md)
|
||||
- [OrbTestLarge](../msg_docs/OrbTestLarge.md)
|
||||
- [FollowTargetEstimator](../msg_docs/FollowTargetEstimator.md)
|
||||
- [CellularStatus](../msg_docs/CellularStatus.md)
|
||||
- [QshellRetval](../msg_docs/QshellRetval.md)
|
||||
- [OrbitStatus](../msg_docs/OrbitStatus.md)
|
||||
- [VehicleStatusV0](../msg_docs/VehicleStatusV0.md)
|
||||
- [FailureDetectorStatus](../msg_docs/FailureDetectorStatus.md)
|
||||
- [LogMessage](../msg_docs/LogMessage.md)
|
||||
- [SatelliteInfo](../msg_docs/SatelliteInfo.md)
|
||||
- [SensorPreflightMag](../msg_docs/SensorPreflightMag.md)
|
||||
- [NavigatorMissionItem](../msg_docs/NavigatorMissionItem.md)
|
||||
- [FixedWingLateralGuidanceStatus](../msg_docs/FixedWingLateralGuidanceStatus.md)
|
||||
- [BatteryStatusV0](../msg_docs/BatteryStatusV0.md)
|
||||
- [EstimatorInnovations](../msg_docs/EstimatorInnovations.md)
|
||||
- [EstimatorStatus](../msg_docs/EstimatorStatus.md)
|
||||
- [NeuralControl](../msg_docs/NeuralControl.md)
|
||||
- [TaskStackInfo](../msg_docs/TaskStackInfo.md)
|
||||
- [RcParameterMap](../msg_docs/RcParameterMap.md)
|
||||
- [SensorSelection](../msg_docs/SensorSelection.md)
|
||||
- [FlightPhaseEstimation](../msg_docs/FlightPhaseEstimation.md)
|
||||
- [ParameterSetValueResponse](../msg_docs/ParameterSetValueResponse.md)
|
||||
- [ActuatorTest](../msg_docs/ActuatorTest.md)
|
||||
- [VehicleImuStatus](../msg_docs/VehicleImuStatus.md)
|
||||
- [MountOrientation](../msg_docs/MountOrientation.md)
|
||||
- [CameraStatus](../msg_docs/CameraStatus.md)
|
||||
- [AutotuneAttitudeControlStatus](../msg_docs/AutotuneAttitudeControlStatus.md)
|
||||
- [FollowTarget](../msg_docs/FollowTarget.md)
|
||||
- [EstimatorGpsStatus](../msg_docs/EstimatorGpsStatus.md)
|
||||
- [ButtonEvent](../msg_docs/ButtonEvent.md)
|
||||
- [DebugArray](../msg_docs/DebugArray.md)
|
||||
- [Ekf2Timestamps](../msg_docs/Ekf2Timestamps.md)
|
||||
- [GimbalManagerSetManualControl](../msg_docs/GimbalManagerSetManualControl.md)
|
||||
- [IridiumsbdStatus](../msg_docs/IridiumsbdStatus.md)
|
||||
- [OpenDroneIdSystem](../msg_docs/OpenDroneIdSystem.md)
|
||||
- [VehicleImu](../msg_docs/VehicleImu.md)
|
||||
- [GpsDump](../msg_docs/GpsDump.md)
|
||||
- [WheelEncoders](../msg_docs/WheelEncoders.md)
|
||||
- [EstimatorEventFlags](../msg_docs/EstimatorEventFlags.md)
|
||||
- [DebugValue](../msg_docs/DebugValue.md)
|
||||
- [SystemPower](../msg_docs/SystemPower.md)
|
||||
- [LandingTargetInnovations](../msg_docs/LandingTargetInnovations.md)
|
||||
- [VehicleOpticalFlow](../msg_docs/VehicleOpticalFlow.md)
|
||||
- [LandingTargetPose](../msg_docs/LandingTargetPose.md)
|
||||
- [OpenDroneIdOperatorId](../msg_docs/OpenDroneIdOperatorId.md)
|
||||
- [VehicleOpticalFlowVel](../msg_docs/VehicleOpticalFlowVel.md)
|
||||
- [RtlStatus](../msg_docs/RtlStatus.md)
|
||||
- [VehicleAcceleration](../msg_docs/VehicleAcceleration.md)
|
||||
- [GimbalControls](../msg_docs/GimbalControls.md)
|
||||
- [ActuatorServosTrim](../msg_docs/ActuatorServosTrim.md)
|
||||
- [FixedWingLateralStatus](../msg_docs/FixedWingLateralStatus.md)
|
||||
- [HeaterStatus](../msg_docs/HeaterStatus.md)
|
||||
- [YawEstimatorStatus](../msg_docs/YawEstimatorStatus.md)
|
||||
- [RcChannels](../msg_docs/RcChannels.md)
|
||||
- [TecsStatus](../msg_docs/TecsStatus.md)
|
||||
- [EstimatorAidSource1d](../msg_docs/EstimatorAidSource1d.md)
|
||||
- [InputRc](../msg_docs/InputRc.md)
|
||||
- [SensorGyroFifo](../msg_docs/SensorGyroFifo.md)
|
||||
- [GeofenceResult](../msg_docs/GeofenceResult.md)
|
||||
- [OpenDroneIdSelfId](../msg_docs/OpenDroneIdSelfId.md)
|
||||
- [UavcanParameterRequest](../msg_docs/UavcanParameterRequest.md)
|
||||
- [ManualControlSwitches](../msg_docs/ManualControlSwitches.md)
|
||||
- [NavigatorStatus](../msg_docs/NavigatorStatus.md)
|
||||
- [CameraTrigger](../msg_docs/CameraTrigger.md)
|
||||
- [EscReport](../msg_docs/EscReport.md)
|
||||
- [EstimatorBias3d](../msg_docs/EstimatorBias3d.md)
|
||||
- [GeofenceStatus](../msg_docs/GeofenceStatus.md)
|
||||
- [GimbalManagerInformation](../msg_docs/GimbalManagerInformation.md)
|
||||
- [ActuatorOutputs](../msg_docs/ActuatorOutputs.md)
|
||||
- [EventV0](../msg_docs/EventV0.md)
|
||||
- [ArmingCheckRequestV0](../msg_docs/ArmingCheckRequestV0.md)
|
||||
- [EstimatorGpsStatus](../msg_docs/EstimatorGpsStatus.md)
|
||||
- [EstimatorBias](../msg_docs/EstimatorBias.md)
|
||||
- [ParameterSetValueResponse](../msg_docs/ParameterSetValueResponse.md)
|
||||
- [LogMessage](../msg_docs/LogMessage.md)
|
||||
- [PowerMonitor](../msg_docs/PowerMonitor.md)
|
||||
- [VehicleConstraints](../msg_docs/VehicleConstraints.md)
|
||||
- [SensorAirflow](../msg_docs/SensorAirflow.md)
|
||||
- [ArmingCheckRequestV0](../msg_docs/ArmingCheckRequestV0.md)
|
||||
- [ActuatorArmed](../msg_docs/ActuatorArmed.md)
|
||||
- [HoverThrustEstimate](../msg_docs/HoverThrustEstimate.md)
|
||||
- [LaunchDetectionStatus](../msg_docs/LaunchDetectionStatus.md)
|
||||
- [DifferentialPressure](../msg_docs/DifferentialPressure.md)
|
||||
- [MagnetometerBiasEstimate](../msg_docs/MagnetometerBiasEstimate.md)
|
||||
- [PwmInput](../msg_docs/PwmInput.md)
|
||||
- [OrbTestMedium](../msg_docs/OrbTestMedium.md)
|
||||
- [QshellReq](../msg_docs/QshellReq.md)
|
||||
- [GeofenceStatus](../msg_docs/GeofenceStatus.md)
|
||||
- [RcChannels](../msg_docs/RcChannels.md)
|
||||
- [Cpuload](../msg_docs/Cpuload.md)
|
||||
- [DebugArray](../msg_docs/DebugArray.md)
|
||||
- [FlightPhaseEstimation](../msg_docs/FlightPhaseEstimation.md)
|
||||
- [Mission](../msg_docs/Mission.md)
|
||||
- [Airspeed](../msg_docs/Airspeed.md)
|
||||
- [LedControl](../msg_docs/LedControl.md)
|
||||
- [HealthReport](../msg_docs/HealthReport.md)
|
||||
- [FixedWingLateralGuidanceStatus](../msg_docs/FixedWingLateralGuidanceStatus.md)
|
||||
- [FigureEightStatus](../msg_docs/FigureEightStatus.md)
|
||||
- [EstimatorInnovations](../msg_docs/EstimatorInnovations.md)
|
||||
- [VehicleImuStatus](../msg_docs/VehicleImuStatus.md)
|
||||
- [VehicleLocalPositionSetpoint](../msg_docs/VehicleLocalPositionSetpoint.md)
|
||||
- [InputRc](../msg_docs/InputRc.md)
|
||||
- [UavcanParameterRequest](../msg_docs/UavcanParameterRequest.md)
|
||||
- [FixedWingRunwayControl](../msg_docs/FixedWingRunwayControl.md)
|
||||
- [SensorCorrection](../msg_docs/SensorCorrection.md)
|
||||
- [ControlAllocatorStatus](../msg_docs/ControlAllocatorStatus.md)
|
||||
- [AirspeedValidatedV0](../msg_docs/AirspeedValidatedV0.md)
|
||||
- [CanInterfaceStatus](../msg_docs/CanInterfaceStatus.md)
|
||||
- [SensorSelection](../msg_docs/SensorSelection.md)
|
||||
- [DeviceInformation](../msg_docs/DeviceInformation.md)
|
||||
- [CameraTrigger](../msg_docs/CameraTrigger.md)
|
||||
- [SensorAccel](../msg_docs/SensorAccel.md)
|
||||
- [ActuatorServosTrim](../msg_docs/ActuatorServosTrim.md)
|
||||
- [SensorsStatusImu](../msg_docs/SensorsStatusImu.md)
|
||||
- [EstimatorBias3d](../msg_docs/EstimatorBias3d.md)
|
||||
- [GimbalManagerStatus](../msg_docs/GimbalManagerStatus.md)
|
||||
- [BatteryStatusV0](../msg_docs/BatteryStatusV0.md)
|
||||
- [OpenDroneIdSelfId](../msg_docs/OpenDroneIdSelfId.md)
|
||||
- [VehicleImu](../msg_docs/VehicleImu.md)
|
||||
- [MissionResult](../msg_docs/MissionResult.md)
|
||||
- [SensorAccelFifo](../msg_docs/SensorAccelFifo.md)
|
||||
- [DistanceSensorModeChangeRequest](../msg_docs/DistanceSensorModeChangeRequest.md)
|
||||
- [SensorPreflightMag](../msg_docs/SensorPreflightMag.md)
|
||||
- [OrbTest](../msg_docs/OrbTest.md)
|
||||
- [PositionControllerLandingStatus](../msg_docs/PositionControllerLandingStatus.md)
|
||||
- [FuelTankStatus](../msg_docs/FuelTankStatus.md)
|
||||
- [OpenDroneIdSystem](../msg_docs/OpenDroneIdSystem.md)
|
||||
- [OrbitStatus](../msg_docs/OrbitStatus.md)
|
||||
- [Px4ioStatus](../msg_docs/Px4ioStatus.md)
|
||||
- [RtlStatus](../msg_docs/RtlStatus.md)
|
||||
- [ButtonEvent](../msg_docs/ButtonEvent.md)
|
||||
- [VehicleLocalPositionV0](../msg_docs/VehicleLocalPositionV0.md)
|
||||
- [DebugValue](../msg_docs/DebugValue.md)
|
||||
- [ParameterSetUsedRequest](../msg_docs/ParameterSetUsedRequest.md)
|
||||
- [RoverSpeedStatus](../msg_docs/RoverSpeedStatus.md)
|
||||
- [SensorHygrometer](../msg_docs/SensorHygrometer.md)
|
||||
- [OpenDroneIdOperatorId](../msg_docs/OpenDroneIdOperatorId.md)
|
||||
- [InternalCombustionEngineStatus](../msg_docs/InternalCombustionEngineStatus.md)
|
||||
- [GpioOut](../msg_docs/GpioOut.md)
|
||||
- [ActuatorTest](../msg_docs/ActuatorTest.md)
|
||||
- [SensorBaro](../msg_docs/SensorBaro.md)
|
||||
- [PositionControllerStatus](../msg_docs/PositionControllerStatus.md)
|
||||
- [PurePursuitStatus](../msg_docs/PurePursuitStatus.md)
|
||||
- [RoverRateStatus](../msg_docs/RoverRateStatus.md)
|
||||
- [TecsStatus](../msg_docs/TecsStatus.md)
|
||||
- [PpsCapture](../msg_docs/PpsCapture.md)
|
||||
- [RaptorStatus](../msg_docs/RaptorStatus.md)
|
||||
- [EventV0](../msg_docs/EventV0.md)
|
||||
- [GpioRequest](../msg_docs/GpioRequest.md)
|
||||
- [FollowTargetEstimator](../msg_docs/FollowTargetEstimator.md)
|
||||
- [MagWorkerData](../msg_docs/MagWorkerData.md)
|
||||
- [FollowTarget](../msg_docs/FollowTarget.md)
|
||||
- [EstimatorAidSource1d](../msg_docs/EstimatorAidSource1d.md)
|
||||
- [GimbalDeviceSetAttitude](../msg_docs/GimbalDeviceSetAttitude.md)
|
||||
- [SensorGnssRelative](../msg_docs/SensorGnssRelative.md)
|
||||
- [ActionRequest](../msg_docs/ActionRequest.md)
|
||||
- [NavigatorMissionItem](../msg_docs/NavigatorMissionItem.md)
|
||||
- [GpsInjectData](../msg_docs/GpsInjectData.md)
|
||||
- [VehicleStatusV0](../msg_docs/VehicleStatusV0.md)
|
||||
- [DronecanNodeStatus](../msg_docs/DronecanNodeStatus.md)
|
||||
- [UlogStream](../msg_docs/UlogStream.md)
|
||||
- [DebugKeyValue](../msg_docs/DebugKeyValue.md)
|
||||
- [NavigatorStatus](../msg_docs/NavigatorStatus.md)
|
||||
- [MountOrientation](../msg_docs/MountOrientation.md)
|
||||
- [RcParameterMap](../msg_docs/RcParameterMap.md)
|
||||
- [AdcReport](../msg_docs/AdcReport.md)
|
||||
- [EstimatorSensorBias](../msg_docs/EstimatorSensorBias.md)
|
||||
- [InternalCombustionEngineControl](../msg_docs/InternalCombustionEngineControl.md)
|
||||
- [MavlinkLog](../msg_docs/MavlinkLog.md)
|
||||
- [VehicleMagnetometer](../msg_docs/VehicleMagnetometer.md)
|
||||
- [GpioConfig](../msg_docs/GpioConfig.md)
|
||||
- [GainCompression](../msg_docs/GainCompression.md)
|
||||
- [DebugVect](../msg_docs/DebugVect.md)
|
||||
- [ArmingCheckReplyV0](../msg_docs/ArmingCheckReplyV0.md)
|
||||
- [VehicleAttitudeSetpointV0](../msg_docs/VehicleAttitudeSetpointV0.md)
|
||||
- [FollowTargetStatus](../msg_docs/FollowTargetStatus.md)
|
||||
- [RtlTimeEstimate](../msg_docs/RtlTimeEstimate.md)
|
||||
- [RoverAttitudeStatus](../msg_docs/RoverAttitudeStatus.md)
|
||||
- [SensorUwb](../msg_docs/SensorUwb.md)
|
||||
- [YawEstimatorStatus](../msg_docs/YawEstimatorStatus.md)
|
||||
- [VelocityLimits](../msg_docs/VelocityLimits.md)
|
||||
- [TrajectorySetpoint6dof](../msg_docs/TrajectorySetpoint6dof.md)
|
||||
- [OpenDroneIdArmStatus](../msg_docs/OpenDroneIdArmStatus.md)
|
||||
- [EscStatus](../msg_docs/EscStatus.md)
|
||||
- [GimbalManagerInformation](../msg_docs/GimbalManagerInformation.md)
|
||||
- [HeaterStatus](../msg_docs/HeaterStatus.md)
|
||||
- [EstimatorSelectorStatus](../msg_docs/EstimatorSelectorStatus.md)
|
||||
- [GeofenceResult](../msg_docs/GeofenceResult.md)
|
||||
- [PowerButtonState](../msg_docs/PowerButtonState.md)
|
||||
- [Rpm](../msg_docs/Rpm.md)
|
||||
- [WheelEncoders](../msg_docs/WheelEncoders.md)
|
||||
- [LoggerStatus](../msg_docs/LoggerStatus.md)
|
||||
- [CellularStatus](../msg_docs/CellularStatus.md)
|
||||
- [TuneControl](../msg_docs/TuneControl.md)
|
||||
- [ConfigOverridesV0](../msg_docs/ConfigOverridesV0.md)
|
||||
- [GimbalManagerSetAttitude](../msg_docs/GimbalManagerSetAttitude.md)
|
||||
- [OrbTestLarge](../msg_docs/OrbTestLarge.md)
|
||||
- [BatteryInfo](../msg_docs/BatteryInfo.md)
|
||||
- [CameraStatus](../msg_docs/CameraStatus.md)
|
||||
- [QshellRetval](../msg_docs/QshellRetval.md)
|
||||
- [SensorMag](../msg_docs/SensorMag.md)
|
||||
- [RateCtrlStatus](../msg_docs/RateCtrlStatus.md)
|
||||
- [TaskStackInfo](../msg_docs/TaskStackInfo.md)
|
||||
- [EstimatorAidSource2d](../msg_docs/EstimatorAidSource2d.md)
|
||||
- [AirspeedWind](../msg_docs/AirspeedWind.md)
|
||||
- [AutotuneAttitudeControlStatus](../msg_docs/AutotuneAttitudeControlStatus.md)
|
||||
- [GimbalDeviceInformation](../msg_docs/GimbalDeviceInformation.md)
|
||||
- [GpsDump](../msg_docs/GpsDump.md)
|
||||
- [SensorTemp](../msg_docs/SensorTemp.md)
|
||||
- [ParameterResetRequest](../msg_docs/ParameterResetRequest.md)
|
||||
- [TiltrotorExtraControls](../msg_docs/TiltrotorExtraControls.md)
|
||||
- [SensorsStatus](../msg_docs/SensorsStatus.md)
|
||||
- [EstimatorStatus](../msg_docs/EstimatorStatus.md)
|
||||
- [FailureDetectorStatus](../msg_docs/FailureDetectorStatus.md)
|
||||
- [VehicleAirData](../msg_docs/VehicleAirData.md)
|
||||
- [ActuatorControlsStatus](../msg_docs/ActuatorControlsStatus.md)
|
||||
- [TakeoffStatus](../msg_docs/TakeoffStatus.md)
|
||||
- [GeneratorStatus](../msg_docs/GeneratorStatus.md)
|
||||
- [SensorGyroFifo](../msg_docs/SensorGyroFifo.md)
|
||||
- [VehicleAngularVelocity](../msg_docs/VehicleAngularVelocity.md)
|
||||
- [LandingGearWheel](../msg_docs/LandingGearWheel.md)
|
||||
- [ParameterSetValueRequest](../msg_docs/ParameterSetValueRequest.md)
|
||||
- [RegisterExtComponentReplyV0](../msg_docs/RegisterExtComponentReplyV0.md)
|
||||
- [RaptorInput](../msg_docs/RaptorInput.md)
|
||||
- [SensorGyro](../msg_docs/SensorGyro.md)
|
||||
- [ParameterUpdate](../msg_docs/ParameterUpdate.md)
|
||||
- [NormalizedUnsignedSetpoint](../msg_docs/NormalizedUnsignedSetpoint.md)
|
||||
- [PositionSetpoint](../msg_docs/PositionSetpoint.md)
|
||||
- [EstimatorStates](../msg_docs/EstimatorStates.md)
|
||||
- [ActuatorOutputs](../msg_docs/ActuatorOutputs.md)
|
||||
- [ManualControlSwitches](../msg_docs/ManualControlSwitches.md)
|
||||
- [UavcanParameterValue](../msg_docs/UavcanParameterValue.md)
|
||||
- [VehicleAngularAccelerationSetpoint](../msg_docs/VehicleAngularAccelerationSetpoint.md)
|
||||
- [EstimatorEventFlags](../msg_docs/EstimatorEventFlags.md)
|
||||
- [SensorGnssStatus](../msg_docs/SensorGnssStatus.md)
|
||||
- [GimbalManagerSetManualControl](../msg_docs/GimbalManagerSetManualControl.md)
|
||||
- [HomePositionV0](../msg_docs/HomePositionV0.md)
|
||||
- [FixedWingLateralStatus](../msg_docs/FixedWingLateralStatus.md)
|
||||
- [SatelliteInfo](../msg_docs/SatelliteInfo.md)
|
||||
- [IrlockReport](../msg_docs/IrlockReport.md)
|
||||
- [Ping](../msg_docs/Ping.md)
|
||||
- [CameraCapture](../msg_docs/CameraCapture.md)
|
||||
- [Vtx](../msg_docs/Vtx.md)
|
||||
- [Ekf2Timestamps](../msg_docs/Ekf2Timestamps.md)
|
||||
- [RegisterExtComponentRequestV0](../msg_docs/RegisterExtComponentRequestV0.md)
|
||||
- [EscReport](../msg_docs/EscReport.md)
|
||||
- [Gripper](../msg_docs/Gripper.md)
|
||||
- [UlogStreamAck](../msg_docs/UlogStreamAck.md)
|
||||
- [SensorGyroFft](../msg_docs/SensorGyroFft.md)
|
||||
- [VehicleRoi](../msg_docs/VehicleRoi.md)
|
||||
- [VehicleAcceleration](../msg_docs/VehicleAcceleration.md)
|
||||
- [NeuralControl](../msg_docs/NeuralControl.md)
|
||||
- [DatamanResponse](../msg_docs/DatamanResponse.md)
|
||||
- [GimbalControls](../msg_docs/GimbalControls.md)
|
||||
- [MavlinkTunnel](../msg_docs/MavlinkTunnel.md)
|
||||
- [EstimatorAidSource3d](../msg_docs/EstimatorAidSource3d.md)
|
||||
- [DatamanRequest](../msg_docs/DatamanRequest.md)
|
||||
- [Event](../msg_docs/Event.md)
|
||||
- [RadioStatus](../msg_docs/RadioStatus.md)
|
||||
- [VehicleOpticalFlowVel](../msg_docs/VehicleOpticalFlowVel.md)
|
||||
- [IridiumsbdStatus](../msg_docs/IridiumsbdStatus.md)
|
||||
|
||||
:::
|
||||
|
||||
@@ -335,7 +335,7 @@ The configuration can be done using the [UXRCE-DDS parameters](../advanced_confi
|
||||
- [UXRCE_DDS_NS_IDX](../advanced_config/parameter_reference.md#UXRCE_DDS_NS_IDX) <Badge type="tip" text="PX4 v1.17" />: Index-based namespace definition.
|
||||
Setting this parameter to any value other than `-1` creates a namespace with the prefix `uav_` and the specified value, e.g. `uav_0`, `uav_1`, etc.
|
||||
See [namespace](#customizing-the-namespace) for methods to define richer or arbitrary namespaces.
|
||||
- [`UXRCE_DDS_FLCTRL`](../advanced_config/parameter_reference.md#UXRCE_DDS_FLCTRL) <Badge type="tip" text="PX4 main" />: Serial port hardware flow control enable.
|
||||
- [`UXRCE_DDS_FLCTRL`](../advanced_config/parameter_reference.md#UXRCE_DDS_FLCTRL) <Badge type="tip" text="main (planned for: PX4 v1.18)" />: Serial port hardware flow control enable.
|
||||
To use hardware flow control, a custom MicroXRCE Agent needs to be adopted. Please refer to [this PR](https://github.com/eProsima/Micro-XRCE-DDS-Agent/pull/407) for the required changes, cherry-pick them on top of the [agent version](#build-run-within-ros-2-workspace) you need to use and then run the agent with the additional `--flow-control` option.
|
||||
|
||||
:::info
|
||||
|
||||
@@ -35,8 +35,8 @@ PX4-Autopilot contains a template for writing a new application (module) that ru
|
||||
|
||||
```cpp
|
||||
WorkItemExample::WorkItemExample() :
|
||||
ModuleParams(nullptr),
|
||||
ScheduledWorkItem(MODULE_NAME, px4::wq_configurations::test1)
|
||||
ModuleParams(nullptr),
|
||||
ScheduledWorkItem(MODULE_NAME, px4::wq_configurations::test1)
|
||||
{
|
||||
}
|
||||
```
|
||||
|
||||
@@ -45,6 +45,26 @@ atxxxx <command> [arguments...]
|
||||
status print status info
|
||||
```
|
||||
|
||||
## auterion_autostarter
|
||||
|
||||
Source: [drivers/auterion_autostarter](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/auterion_autostarter)
|
||||
|
||||
### Опис
|
||||
|
||||
Driver for starting and auto-detecting different power monitors.
|
||||
|
||||
### Usage {#auterion_autostarter_usage}
|
||||
|
||||
```
|
||||
auterion_autostarter <command> [arguments...]
|
||||
Commands:
|
||||
start
|
||||
|
||||
stop
|
||||
|
||||
status print status info
|
||||
```
|
||||
|
||||
## batmon
|
||||
|
||||
Source: [drivers/smart_battery/batmon](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/smart_battery/batmon)
|
||||
@@ -925,26 +945,6 @@ pca9685_pwm_out <command> [arguments...]
|
||||
status print status info
|
||||
```
|
||||
|
||||
## pm_selector_auterion
|
||||
|
||||
Source: [drivers/power_monitor/pm_selector_auterion](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/power_monitor/pm_selector_auterion)
|
||||
|
||||
### Опис
|
||||
|
||||
Driver for starting and auto-detecting different power monitors.
|
||||
|
||||
### Usage {#pm_selector_auterion_usage}
|
||||
|
||||
```
|
||||
pm_selector_auterion <command> [arguments...]
|
||||
Commands:
|
||||
start
|
||||
|
||||
stop
|
||||
|
||||
status print status info
|
||||
```
|
||||
|
||||
## pmw3901
|
||||
|
||||
Source: [drivers/optical_flow/pmw3901](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/optical_flow/pmw3901)
|
||||
@@ -1109,7 +1109,7 @@ px4io <command> [arguments...]
|
||||
|
||||
## rgbled
|
||||
|
||||
Source: [drivers/lights/rgbled_ncp5623c](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/lights/rgbled_ncp5623c)
|
||||
Source: [drivers/lights/rgbled](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/lights/rgbled)
|
||||
|
||||
### Usage {#rgbled_usage}
|
||||
|
||||
@@ -1124,9 +1124,7 @@ rgbled <command> [arguments...]
|
||||
[-f <val>] bus frequency in kHz
|
||||
[-q] quiet startup (no message if no device found)
|
||||
[-a <val>] I2C address
|
||||
default: 57
|
||||
[-o <val>] RGB PWM Assignment
|
||||
default: 123
|
||||
default: 85
|
||||
|
||||
stop
|
||||
|
||||
@@ -1438,6 +1436,30 @@ tap_esc <command> [arguments...]
|
||||
default: 4
|
||||
```
|
||||
|
||||
## tmp102
|
||||
|
||||
Source: [drivers/temperature_sensor/tmp102](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/temperature_sensor/tmp102)
|
||||
|
||||
### Usage {#tmp102_usage}
|
||||
|
||||
```
|
||||
tmp102 <command> [arguments...]
|
||||
Commands:
|
||||
start
|
||||
[-I] Internal I2C bus(es)
|
||||
[-X] External I2C bus(es)
|
||||
[-b <val>] board-specific bus (default=all) (external SPI: n-th bus
|
||||
(default=1))
|
||||
[-f <val>] bus frequency in kHz
|
||||
[-q] quiet startup (no message if no device found)
|
||||
[-a <val>] I2C address
|
||||
default: 72
|
||||
|
||||
stop
|
||||
|
||||
status print status info
|
||||
```
|
||||
|
||||
## tone_alarm
|
||||
|
||||
Source: [drivers/tone_alarm](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/tone_alarm)
|
||||
@@ -1627,6 +1649,76 @@ voxlpm [arguments...]
|
||||
status print status info
|
||||
```
|
||||
|
||||
## vtx
|
||||
|
||||
Source: [drivers/vtx](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/vtx)
|
||||
|
||||
### Опис
|
||||
|
||||
This module communicates with a VTX camera via serial port. It can be used to
|
||||
configure the camera settings and to control the camera's video transmission.
|
||||
Supported protocols are:
|
||||
|
||||
- SmartAudio v1, v2.0, v2.1
|
||||
- Tramp
|
||||
|
||||
### Usage {#vtx_usage}
|
||||
|
||||
```
|
||||
vtx <command> [arguments...]
|
||||
Commands:
|
||||
start
|
||||
-d <val> VTX device
|
||||
values: <file:dev>
|
||||
|
||||
<int> Sets an entry in the mapping table: <index> <aux channel>
|
||||
<band> <channel> <power level> <start range> <end range>
|
||||
|
||||
stop
|
||||
|
||||
status print status info
|
||||
```
|
||||
|
||||
## vtxtable
|
||||
|
||||
Source: [drivers/vtxtable](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/vtxtable)
|
||||
|
||||
### Опис
|
||||
|
||||
Manages the VTX frequency, power level and RC mapping table for VTX configuration.
|
||||
|
||||
### Usage {#vtxtable_usage}
|
||||
|
||||
```
|
||||
vtxtable <command> [arguments...]
|
||||
Commands:
|
||||
status Shows the current VTX table configuration.
|
||||
|
||||
name Sets the VTX table name: <string>
|
||||
|
||||
bands Sets the number of bands: <int>
|
||||
|
||||
band Sets the band frequencies: <1-index> <name> <letter>
|
||||
<attribute> <frequencies...>
|
||||
|
||||
channels Sets the number of channels: <int>
|
||||
|
||||
powerlevels Sets number of power levels: <int>
|
||||
|
||||
powervalues Sets the power level values: <int...>
|
||||
|
||||
powerlabels Sets the power level labels: <3 chars...>
|
||||
|
||||
<int> Sets an entry in the mapping table: <0-index> <aux channel>
|
||||
<band> <channel> <power level> <start range> <end range>
|
||||
|
||||
clear Clears the VTX table configuration.
|
||||
|
||||
save Saves the VTX config to a file: <file>
|
||||
|
||||
load Loads the VTX config from a file: <file>
|
||||
```
|
||||
|
||||
## zenoh
|
||||
|
||||
Source: [modules/zenoh](https://github.com/PX4/PX4-Autopilot/tree/main/src/modules/zenoh)
|
||||
|
||||
@@ -1,5 +1,36 @@
|
||||
# Modules Reference: Template
|
||||
|
||||
## mc_raptor
|
||||
|
||||
Source: [modules/mc_raptor](https://github.com/PX4/PX4-Autopilot/tree/main/src/modules/mc_raptor)
|
||||
|
||||
### Опис
|
||||
|
||||
RAPTOR Policy Flight Mode
|
||||
|
||||
### Usage {#mc_raptor_usage}
|
||||
|
||||
```
|
||||
mc_raptor <command> [arguments...]
|
||||
Commands:
|
||||
start
|
||||
|
||||
intref Modify internal reference
|
||||
lissajous Set Lissajous trajectory parameters
|
||||
<A> Amplitude X [m]
|
||||
<B> Amplitude Y [m]
|
||||
<C> Amplitude Z [m]
|
||||
<fa> Frequency a
|
||||
<fb> Frequency b
|
||||
<fc> Frequency c
|
||||
<duration> Total duration [s]
|
||||
<ramp> Ramp duration [s]
|
||||
|
||||
stop
|
||||
|
||||
status print status info
|
||||
```
|
||||
|
||||
## module
|
||||
|
||||
Source: [templates/template_module](https://github.com/PX4/PX4-Autopilot/tree/main/src/templates/template_module)
|
||||
|
||||
@@ -1,12 +1,57 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ActionRequest (повідомлення UORB)
|
||||
|
||||
Action request for the vehicle's main state
|
||||
Action request for the vehicle's main state.
|
||||
|
||||
Message represents actions requested by a PX4 internal component towards the main state machine such as a request to arm or switch mode.
|
||||
It allows mapping triggers from various external interfaces like RC channels or MAVLink to cause an action.
|
||||
Request are published by `manual_control` and subscribed by the `commander` and `vtol_att_control` modules.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActionRequest.msg)
|
||||
**TOPICS:** action_request
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| --------- | -------- | ---------------------------------------------------------------- | ----------------- | ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| action | `uint8` | | [ACTION](#ACTION) | Requested action |
|
||||
| source | `uint8` | | [SOURCE](#SOURCE) | Request trigger type, such as a switch, button or gesture |
|
||||
| mode | `uint8` | | | Requested mode. Only applies when `action` is `ACTION_SWITCH_MODE`. Values for this field are defined by the `vehicle_status_s::NAVIGATION_STATE_*` enumeration. |
|
||||
|
||||
## Enums
|
||||
|
||||
### ACTION {#ACTION}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ---------------------------------------------------------------------------------------- |
|
||||
| <a href="#ACTION_DISARM"></a> ACTION_DISARM | `uint8` | 0 | Disarm vehicle |
|
||||
| <a href="#ACTION_ARM"></a> ACTION_ARM | `uint8` | 1 | Arm vehicle |
|
||||
| <a href="#ACTION_TOGGLE_ARMING"></a> ACTION_TOGGLE_ARMING | `uint8` | 2 | Toggle arming |
|
||||
| <a href="#ACTION_UNKILL"></a> ACTION_UNKILL | `uint8` | 3 | Revert a kill action |
|
||||
| <a href="#ACTION_KILL"></a> ACTION_KILL | `uint8` | 4 | Kill vehicle (instantly stop the motors) |
|
||||
| <a href="#ACTION_SWITCH_MODE"></a> ACTION_SWITCH_MODE | `uint8` | 5 | Switch mode. The target mode is set in the `mode` field. |
|
||||
| <a href="#ACTION_VTOL_TRANSITION_TO_MULTICOPTER"></a> ACTION_VTOL_TRANSITION_TO_MULTICOPTER | `uint8` | 6 | Transition to hover flight |
|
||||
| <a href="#ACTION_VTOL_TRANSITION_TO_FIXEDWING"></a> ACTION_VTOL_TRANSITION_TO_FIXEDWING | `uint8` | 7 | Transition to fast forward flight |
|
||||
| <a href="#ACTION_TERMINATION"></a> ACTION_TERMINATION | `uint8` | 8 | Irreversibly output failsafe values on all outputs, trigger parachute |
|
||||
|
||||
### SOURCE {#SOURCE}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ---------------------------------------------------------------------------------------------------------------------- | ------- | -------- | --------------------------------------------------------------- |
|
||||
| <a href="#SOURCE_STICK_GESTURE"></a> SOURCE_STICK_GESTURE | `uint8` | 0 | Triggered by holding the sticks in a certain position |
|
||||
| <a href="#SOURCE_RC_SWITCH"></a> SOURCE_RC_SWITCH | `uint8` | 1 | Triggered by an RC switch moving into a certain position |
|
||||
| <a href="#SOURCE_RC_BUTTON"></a> SOURCE_RC_BUTTON | `uint8` | 2 | Triggered by a momentary button on the RC being pressed or held |
|
||||
| <a href="#SOURCE_RC_MODE_SLOT"></a> SOURCE_RC_MODE_SLOT | `uint8` | 3 | Mode change through the RC mode selection mechanism |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActionRequest.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Action request for the vehicle's main state
|
||||
@@ -35,5 +80,6 @@ uint8 SOURCE_RC_BUTTON = 2 # Triggered by a momentary button on the RC bein
|
||||
uint8 SOURCE_RC_MODE_SLOT = 3 # Mode change through the RC mode selection mechanism
|
||||
|
||||
uint8 mode # Requested mode. Only applies when `action` is `ACTION_SWITCH_MODE`. Values for this field are defined by the `vehicle_status_s::NAVIGATION_STATE_*` enumeration.
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,30 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ActuatorArmed (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActuatorArmed.msg)
|
||||
**TOPICS:** actuator_armed
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| -------------------------------------------------------------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | -------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| armed | `bool` | | | Set to true if system is armed |
|
||||
| prearmed | `bool` | | | Set to true if the actuator safety is disabled but motors are not armed |
|
||||
| ready_to_arm | `bool` | | | Set to true if system is ready to be armed |
|
||||
| lockdown | `bool` | | | Set to true if actuators are forced to being disabled (due to emergency or HIL) |
|
||||
| kill | `bool` | | | Set to true if manual throttle kill switch is engaged |
|
||||
| termination | `bool` | | | Send out failsafe (by default same as disarmed) output |
|
||||
| in_esc_calibration_mode | `bool` | | | IO/FMU should ignore messages from the actuator controls topics |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActuatorArmed.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -12,5 +36,6 @@ bool lockdown # Set to true if actuators are forced to being disabled (due to e
|
||||
bool kill # Set to true if manual throttle kill switch is engaged
|
||||
bool termination # Send out failsafe (by default same as disarmed) output
|
||||
bool in_esc_calibration_mode # IO/FMU should ignore messages from the actuator controls topics
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,24 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ActuatorControlsStatus (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActuatorControlsStatus.msg)
|
||||
**TOPICS:** actuator_controls_status_0 actuator_controls_status_1
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ---------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| control_power | `float32[3]` | | | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActuatorControlsStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -8,5 +26,6 @@ uint64 timestamp # time since system start (microseconds)
|
||||
float32[3] control_power
|
||||
|
||||
# TOPICS actuator_controls_status_0 actuator_controls_status_1
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,11 +1,39 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ActuatorMotors (повідомлення UORB)
|
||||
|
||||
Повідомлення про керування двигуном
|
||||
Motor control message.
|
||||
|
||||
Normalised thrust setpoint for up to 12 motors.
|
||||
Published by the vehicle's allocation and consumed by the ESC protocol drivers e.g. PWM, DSHOT, UAVCAN.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/ActuatorMotors.msg)
|
||||
**TOPICS:** actuator_motors
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------- | ------------- | ---------------------------------------------------------------- | ---------------------------------------------------------------------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| timestamp_sample | `uint64` | us | | Sampling timestamp of the data this control response is based on |
|
||||
| reversible_flags | `uint16` | | | Bitset indicating which motors are configured to be reversible |
|
||||
| control | `float32[12]` | | [-1 : 1] | Normalized thrust. where 1 means maximum positive thrust, -1 maximum negative (if not supported by the output, <0 maps to NaN). NaN maps to disarmed (stop the motors) |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ----------------------------------------------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR1"></a> ACTUATOR_FUNCTION_MOTOR1 | `uint8` | 101 | |
|
||||
| <a href="#NUM_CONTROLS"></a> NUM_CONTROLS | `uint8` | 12 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/ActuatorMotors.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Motor control message
|
||||
@@ -24,5 +52,6 @@ uint8 ACTUATOR_FUNCTION_MOTOR1 = 101 #
|
||||
|
||||
uint8 NUM_CONTROLS = 12 #
|
||||
float32[12] control # [@range -1, 1] Normalized thrust. where 1 means maximum positive thrust, -1 maximum negative (if not supported by the output, <0 maps to NaN). NaN maps to disarmed (stop the motors)
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,32 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ActuatorOutputs (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActuatorOutputs.msg)
|
||||
**TOPICS:** actuator_outputs actuator_outputs_sim actuator_outputs_debug
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| --------- | ------------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| noutputs | `uint32` | | | valid outputs |
|
||||
| output | `float32[16]` | | | output data, in natural output units |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ------------------- |
|
||||
| <a href="#NUM_ACTUATOR_OUTPUTS"></a> NUM_ACTUATOR_OUTPUTS | `uint8` | 16 | |
|
||||
| <a href="#NUM_ACTUATOR_OUTPUT_GROUPS "></a> NUM_ACTUATOR_OUTPUT_GROUPS | `uint8` | 4 | for sanity checking |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActuatorOutputs.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -11,5 +37,6 @@ float32[16] output # output data, in natural output units
|
||||
|
||||
# actuator_outputs_sim is used for SITL, HITL & SIH (with an output range of [-1, 1])
|
||||
# TOPICS actuator_outputs actuator_outputs_sim actuator_outputs_debug
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,11 +1,37 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ActuatorServos (повідомлення UORB)
|
||||
|
||||
Повідомлення про керування сервоприводом
|
||||
Servo control message.
|
||||
|
||||
Normalised output setpoint for up to 8 servos.
|
||||
Published by the vehicle's allocation and consumed by the actuator output drivers.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/ActuatorServos.msg)
|
||||
**TOPICS:** actuator_servos
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------------------------------------------------------------------------- | ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| timestamp_sample | `uint64` | us | | Sampling timestamp of the data this control response is based on |
|
||||
| control | `float32[8]` | | [-1 : 1] | Normalized output. 1 means maximum positive position. -1 maximum negative position (if not supported by the output, <0 maps to NaN). NaN maps to disarmed. |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0 | |
|
||||
| <a href="#NUM_CONTROLS"></a> NUM_CONTROLS | `uint8` | 8 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/ActuatorServos.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Servo control message
|
||||
@@ -20,5 +46,6 @@ uint64 timestamp_sample # [us] Sampling timestamp of the data this control resp
|
||||
|
||||
uint8 NUM_CONTROLS = 8 #
|
||||
float32[8] control # [-] [@range -1, 1] Normalized output. 1 means maximum positive position. -1 maximum negative position (if not supported by the output, <0 maps to NaN). NaN maps to disarmed.
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,8 +1,32 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ActuatorServosTrim (повідомлення UORB)
|
||||
|
||||
Підлаштування сервоприводів, що додаються як зміщення до виходів сервоприводів
|
||||
Servo trims, added as offset to servo outputs.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActuatorServosTrim.msg)
|
||||
**TOPICS:** actuator_servostrim
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| --------- | ------------ | ---------------------------------------------------------------- | ---------- | ---------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| trim | `float32[8]` | | | range: [-1, 1] |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------- | ------- | -------- | ---- |
|
||||
| <a href="#NUM_CONTROLS"></a> NUM_CONTROLS | `uint8` | 8 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActuatorServosTrim.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Servo trims, added as offset to servo outputs
|
||||
@@ -10,5 +34,6 @@ uint64 timestamp # time since system start (microseconds)
|
||||
|
||||
uint8 NUM_CONTROLS = 8
|
||||
float32[8] trim # range: [-1, 1]
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,39 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ActuatorTest (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActuatorTest.msg)
|
||||
**TOPICS:** actuator_test
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | -------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| action | `uint8` | | | one of ACTION\_\* |
|
||||
| function | `uint16` | | | actuator output function |
|
||||
| value | `float32` | | | range: [-1, 1], where 1 means maximum positive output, |
|
||||
| timeout_ms | `uint32` | | | timeout in ms after which to exit test mode (if 0, do not time out) |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------------------- | ------- | -------- | -------------------------------------------------------------------------------------------------------------------- |
|
||||
| <a href="#ACTION_RELEASE_CONTROL"></a> ACTION_RELEASE_CONTROL | `uint8` | 0 | exit test mode for the given function |
|
||||
| <a href="#ACTION_DO_CONTROL"></a> ACTION_DO_CONTROL | `uint8` | 1 | enable actuator test mode |
|
||||
| <a href="#FUNCTION_MOTOR1"></a> FUNCTION_MOTOR1 | `uint8` | 101 | |
|
||||
| <a href="#MAX_NUM_MOTORS"></a> MAX_NUM_MOTORS | `uint8` | 12 | |
|
||||
| <a href="#FUNCTION_SERVO1"></a> FUNCTION_SERVO1 | `uint8` | 201 | |
|
||||
| <a href="#MAX_NUM_SERVOS"></a> MAX_NUM_SERVOS | `uint8` | 8 | |
|
||||
| <a href="#ORB_QUEUE_LENGTH"></a> ORB_QUEUE_LENGTH | `uint8` | 16 | > = MAX_NUM_MOTORS to support code in esc_calibration |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ActuatorTest.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -24,5 +57,6 @@ float32 value # range: [-1, 1], where 1 means maximum positive output,
|
||||
uint32 timeout_ms # timeout in ms after which to exit test mode (if 0, do not time out)
|
||||
|
||||
uint8 ORB_QUEUE_LENGTH = 16 # >= MAX_NUM_MOTORS to support code in esc_calibration
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,10 +1,32 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# AdcReport (повідомлення UORB)
|
||||
|
||||
ADC raw data.
|
||||
|
||||
Communicates raw data from an analog-to-digital converter (ADC) to other modules, such as battery status.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/AdcReport.msg)
|
||||
**TOPICS:** adc_report
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------- | ----------- | ---------------------------------------------------------------- | ---------- | ---------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| device_id | `uint32` | | | unique device ID for the sensor that does not change between power cycles |
|
||||
| channel_id | `int16[16]` | | | ADC channel IDs, negative for non-existent, TODO: should be kept same as array index |
|
||||
| raw_data | `int32[16]` | | | ADC channel raw value, accept negative value, valid if channel ID is positive |
|
||||
| resolution | `uint32` | | | ADC channel resolution |
|
||||
| v_ref | `float32` | V | | ADC channel voltage reference, use to calculate LSB voltage(lsb=scale/resolution) |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/AdcReport.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# ADC raw data.
|
||||
@@ -17,5 +39,6 @@ int16[16] channel_id # [-] ADC channel IDs, negative for non-existent, TODO: sh
|
||||
int32[16] raw_data # [-] ADC channel raw value, accept negative value, valid if channel ID is positive
|
||||
uint32 resolution # [-] ADC channel resolution
|
||||
float32 v_ref # [V] ADC channel voltage reference, use to calculate LSB voltage(lsb=scale/resolution)
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,11 +1,32 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# Airspeed (повідомлення UORB)
|
||||
|
||||
Airspeed data from sensors
|
||||
Airspeed data from sensors.
|
||||
|
||||
This is published by airspeed sensor drivers, CAN airspeed sensors, simulators.
|
||||
It is subscribed by the airspeed selector module, which validates the data from multiple sensors and passes on a single estimation to the EKF, controllers and telemetry providers.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/Airspeed.msg)
|
||||
**TOPICS:** airspeed
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | --------------------------------------------------------------------------- | -------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| timestamp_sample | `uint64` | us | | Timestamp of the raw data |
|
||||
| indicated_airspeed_m_s | `float32` | m/s | | Indicated airspeed |
|
||||
| true_airspeed_m_s | `float32` | m/s | | True airspeed |
|
||||
| confidence | `float32` | | [0 : 1] | Confidence value for this sensor |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/Airspeed.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Airspeed data from sensors
|
||||
@@ -18,5 +39,6 @@ uint64 timestamp_sample # [us] Timestamp of the raw data
|
||||
float32 indicated_airspeed_m_s # [m/s] Indicated airspeed
|
||||
float32 true_airspeed_m_s # [m/s] True airspeed
|
||||
float32 confidence # [@range 0,1] Confidence value for this sensor
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,11 +1,56 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# AirspeedValidated (повідомлення UORB)
|
||||
|
||||
Validated airspeed
|
||||
Validated airspeed.
|
||||
|
||||
Provides information about airspeed (indicated, true, calibrated) and the source of the data.
|
||||
Used by controllers, estimators and for airspeed reporting to operator.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/AirspeedValidated.msg)
|
||||
**TOPICS:** airspeed_validated
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ----------------------------------------------------------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ----------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| indicated_airspeed_m_s | `float32` | m/s | | Indicated airspeed (IAS) (Invalid: NaN) |
|
||||
| calibrated_airspeed_m_s | `float32` | m/s | | Calibrated airspeed (CAS) (Invalid: NaN) |
|
||||
| true_airspeed_m_s | `float32` | m/s | | True airspeed (TAS) (Invalid: NaN) |
|
||||
| airspeed_source | `int8` | | [SOURCE](#SOURCE) | Source of currently published airspeed values |
|
||||
| calibrated_ground_minus_wind_m_s | `float32` | m/s | | CAS calculated from groundspeed - windspeed, where windspeed is estimated based on a zero-sideslip assumption (Invalid: NaN) |
|
||||
| calibraded_airspeed_synth_m_s | `float32` | m/s | | Synthetic airspeed (Invalid: NaN) |
|
||||
| airspeed_derivative_filtered | `float32` | m/s^2 | | Filtered indicated airspeed derivative |
|
||||
| throttle_filtered | `float32` | | | Filtered fixed-wing throttle |
|
||||
| pitch_filtered | `float32` | rad | | Filtered pitch |
|
||||
|
||||
## Enums
|
||||
|
||||
### SOURCE {#SOURCE}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------------------------------------------------------------------- | ------ | -------- | ----------------------- |
|
||||
| <a href="#SOURCE_DISABLED"></a> SOURCE_DISABLED | `int8` | -1 | Disabled |
|
||||
| <a href="#SOURCE_GROUND_MINUS_WIND"></a> SOURCE_GROUND_MINUS_WIND | `int8` | 0 | Ground speed minus wind |
|
||||
| <a href="#SOURCE_SENSOR_1"></a> SOURCE_SENSOR_1 | `int8` | 1 | Sensor 1 |
|
||||
| <a href="#SOURCE_SENSOR_2"></a> SOURCE_SENSOR_2 | `int8` | 2 | Sensor 2 |
|
||||
| <a href="#SOURCE_SENSOR_3"></a> SOURCE_SENSOR_3 | `int8` | 3 | Sensor 3 |
|
||||
| <a href="#SOURCE_SYNTHETIC"></a> SOURCE_SYNTHETIC | `int8` | 4 | Synthetic airspeed |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 1 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/AirspeedValidated.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Validated airspeed
|
||||
@@ -35,5 +80,6 @@ float32 calibraded_airspeed_synth_m_s # [m/s] [@invalid NaN] Synthetic airsp
|
||||
float32 airspeed_derivative_filtered # [m/s^2] Filtered indicated airspeed derivative
|
||||
float32 throttle_filtered # [-] Filtered fixed-wing throttle
|
||||
float32 pitch_filtered # [rad] Filtered pitch
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,39 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# AirspeedValidatedV0 (UORB message)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/AirspeedValidatedV0.msg)
|
||||
**TOPICS:** airspeed_validatedv0
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ----------------------------------------------------------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | ------------------------------------------------------------------------------------------------------------------------------------ |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| indicated_airspeed_m_s | `float32` | | | indicated airspeed in m/s (IAS), set to NAN if invalid |
|
||||
| calibrated_airspeed_m_s | `float32` | | | calibrated airspeed in m/s (CAS, accounts for instrumentation errors), set to NAN if invalid |
|
||||
| true_airspeed_m_s | `float32` | | | true filtered airspeed in m/s (TAS), set to NAN if invalid |
|
||||
| calibrated_ground_minus_wind_m_s | `float32` | | | CAS calculated from groundspeed - windspeed, where windspeed is estimated based on a zero-sideslip assumption, set to NAN if invalid |
|
||||
| true_ground_minus_wind_m_s | `float32` | | | TAS calculated from groundspeed - windspeed, where windspeed is estimated based on a zero-sideslip assumption, set to NAN if invalid |
|
||||
| airspeed_sensor_measurement_valid | `bool` | | | True if data from at least one airspeed sensor is declared valid. |
|
||||
| selected_airspeed_index | `int8` | | | 1-3: airspeed sensor index, 0: groundspeed-windspeed, -1: airspeed invalid |
|
||||
| airspeed_derivative_filtered | `float32` | | | filtered indicated airspeed derivative [m/s/s] |
|
||||
| throttle_filtered | `float32` | | | filtered fixed-wing throttle [-] |
|
||||
| pitch_filtered | `float32` | | | filtered pitch [rad] |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/AirspeedValidatedV0.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint32 MESSAGE_VERSION = 0
|
||||
@@ -21,5 +54,6 @@ int8 selected_airspeed_index # 1-3: airspeed sensor index, 0: groundspeed-win
|
||||
float32 airspeed_derivative_filtered # filtered indicated airspeed derivative [m/s/s]
|
||||
float32 throttle_filtered # filtered fixed-wing throttle [-]
|
||||
float32 pitch_filtered # filtered pitch [rad]
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,10 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# AirspeedWind (повідомлення UORB)
|
||||
|
||||
Wind estimate (from airspeed_selector)
|
||||
Wind estimate (from airspeed_selector).
|
||||
|
||||
Contains wind estimation and airspeed innovation information estimated by the WindEstimator
|
||||
in the airspeed selector module.
|
||||
@@ -8,7 +12,42 @@ in the airspeed selector module.
|
||||
This message is published by the airspeed selector for debugging purposes, and is not
|
||||
subscribed to by any other modules.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/AirspeedWind.msg)
|
||||
**TOPICS:** airspeed_wind
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| -------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | -------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| timestamp_sample | `uint64` | us | | Timestamp of the raw data |
|
||||
| windspeed_north | `float32` | m/s | | Wind component in north / X direction |
|
||||
| windspeed_east | `float32` | m/s | | Wind component in east / Y direction |
|
||||
| variance_north | `float32` | (m/s)^2 | | Wind estimate error variance in north / X direction (Invalid: 0 if not estimated) |
|
||||
| variance_east | `float32` | (m/s)^2 | | Wind estimate error variance in east / Y direction (Invalid: 0 if not estimated) |
|
||||
| tas_innov | `float32` | m/s | | True airspeed innovation |
|
||||
| tas_innov_var | `float32` | m/s | | True airspeed innovation variance |
|
||||
| tas_scale_raw | `float32` | | | Estimated true airspeed scale factor (not validated) |
|
||||
| tas_scale_raw_var | `float32` | | | True airspeed scale factor variance |
|
||||
| tas_scale_validated | `float32` | | | Estimated true airspeed scale factor after validation |
|
||||
| beta_innov | `float32` | rad | | Sideslip measurement innovation |
|
||||
| beta_innov_var | `float32` | rad^2 | | Sideslip measurement innovation variance |
|
||||
| source | `uint8` | | | source of wind estimate |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ---------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ----------------------------------------------------------------------------------------------------- |
|
||||
| <a href="#SOURCE_AS_BETA_ONLY"></a> SOURCE_AS_BETA_ONLY | `uint8` | 0 | Wind estimate only based on synthetic sideslip fusion |
|
||||
| <a href="#SOURCE_AS_SENSOR_1"></a> SOURCE_AS_SENSOR_1 | `uint8` | 1 | Combined synthetic sideslip and airspeed fusion (data from first airspeed sensor) |
|
||||
| <a href="#SOURCE_AS_SENSOR_2"></a> SOURCE_AS_SENSOR_2 | `uint8` | 2 | Combined synthetic sideslip and airspeed fusion (data from second airspeed sensor) |
|
||||
| <a href="#SOURCE_AS_SENSOR_3"></a> SOURCE_AS_SENSOR_3 | `uint8` | 3 | Combined synthetic sideslip and airspeed fusion (data from third airspeed sensor) |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/AirspeedWind.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Wind estimate (from airspeed_selector)
|
||||
@@ -45,5 +84,6 @@ uint8 SOURCE_AS_BETA_ONLY = 0 # Wind estimate only based on synthetic sideslip f
|
||||
uint8 SOURCE_AS_SENSOR_1 = 1 # Combined synthetic sideslip and airspeed fusion (data from first airspeed sensor)
|
||||
uint8 SOURCE_AS_SENSOR_2 = 2 # Combined synthetic sideslip and airspeed fusion (data from second airspeed sensor)
|
||||
uint8 SOURCE_AS_SENSOR_3 = 3 # Combined synthetic sideslip and airspeed fusion (data from third airspeed sensor)
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,10 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ArmingCheckReply (повідомлення UORB)
|
||||
|
||||
Arming check reply
|
||||
Arming check reply.
|
||||
|
||||
This is a response to an ArmingCheckRequest message sent by the FMU to an external component, such as a ROS 2 navigation mode.
|
||||
The response contains the current set of external mode requirements, and a queue of events indicating recent failures to set the mode (which the FMU may then forward to a ground station).
|
||||
@@ -9,7 +13,55 @@ The request is sent regularly to all registered ROS modes, even while armed, so
|
||||
Note that the external component is identified by its registration_id, which is allocated to the component during registration (arming_check_id in RegisterExtComponentReply).
|
||||
The message is not used by internal/FMU components, as their mode requirements are known at compile time.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/ArmingCheckReply.msg)
|
||||
**TOPICS:** arming_checkreply
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| -------------------------------------------------------------------------------------------------------------------- | ---------- | ---------------------------------------------------------------- | ------------------------------------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start. |
|
||||
| request_id | `uint8` | | | Id of ArmingCheckRequest for which this is a response |
|
||||
| registration_id | `uint8` | | | Id of external component emitting this response |
|
||||
| health_component_index | `uint8` | | [HEALTH_COMPONENT_INDEX](#HEALTH_COMPONENT_INDEX) | |
|
||||
| health_component_is_present | `bool` | | | Unused. Intended for use with health events interface (health_component_t in events.json) |
|
||||
| health_component_warning | `bool` | | | Unused. Intended for use with health events interface (health_component_t in events.json) |
|
||||
| health_component_error | `bool` | | | Unused. Intended for use with health events interface (health_component_t in events.json) |
|
||||
| can_arm_and_run | `bool` | | | True if the component can arm. For navigation mode components, true if the component can arm in the mode or switch to the mode when already armed |
|
||||
| num_events | `uint8` | | | Number of queued failure messages (Event) in the events field |
|
||||
| events | `Event[5]` | | | Arming failure reasons (Queue of events to report to GCS) |
|
||||
| mode_req_angular_velocity | `bool` | | | Requires angular velocity estimate (e.g. from gyroscope) |
|
||||
| mode_req_attitude | `bool` | | | Requires an attitude estimate |
|
||||
| mode_req_local_alt | `bool` | | | Requires a local altitude estimate |
|
||||
| mode_req_local_position | `bool` | | | Requires a local position estimate |
|
||||
| mode_req_local_position_relaxed | `bool` | | | Requires a more relaxed global position estimate |
|
||||
| mode_req_global_position | `bool` | | | Requires a global position estimate |
|
||||
| mode_req_global_position_relaxed | `bool` | | | Requires a relaxed global position estimate |
|
||||
| mode_req_mission | `bool` | | | Requires an uploaded mission |
|
||||
| mode_req_home_position | `bool` | | | Requires a home position (such as RTL/Return mode) |
|
||||
| mode_req_prevent_arming | `bool` | | | Prevent arming (such as in Land mode) |
|
||||
| mode_req_manual_control | `bool` | | | Requires a manual controller |
|
||||
|
||||
## Enums
|
||||
|
||||
### HEALTH_COMPONENT_INDEX {#HEALTH_COMPONENT_INDEX}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | --------------------------------------------------------- |
|
||||
| <a href="#HEALTH_COMPONENT_INDEX_NONE"></a> HEALTH_COMPONENT_INDEX_NONE | `uint8` | 0 | Index of health component for which this response applies |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 1 | |
|
||||
| <a href="#ORB_QUEUE_LENGTH"></a> ORB_QUEUE_LENGTH | `uint8` | 4 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/ArmingCheckReply.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Arming check reply
|
||||
@@ -55,5 +107,6 @@ bool mode_req_prevent_arming # Prevent arming (such as in Land mode)
|
||||
bool mode_req_manual_control # Requires a manual controller
|
||||
|
||||
uint8 ORB_QUEUE_LENGTH = 4
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,50 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ArmingCheckReplyV0 (UORB message)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/ArmingCheckReplyV0.msg)
|
||||
**TOPICS:** arming_checkreplyv0
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------------------------------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | ------------------------------------------------------------------------ |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| request_id | `uint8` | | | |
|
||||
| registration_id | `uint8` | | | |
|
||||
| health_component_index | `uint8` | | | HEALTH_COMPONENT_INDEX_\* |
|
||||
| health_component_is_present | `bool` | | | |
|
||||
| health_component_warning | `bool` | | | |
|
||||
| health_component_error | `bool` | | | |
|
||||
| can_arm_and_run | `bool` | | | whether arming is possible, and if it's a navigation mode, if it can run |
|
||||
| num_events | `uint8` | | | |
|
||||
| events | `EventV0[5]` | | | |
|
||||
| mode_req_angular_velocity | `bool` | | | |
|
||||
| mode_req_attitude | `bool` | | | |
|
||||
| mode_req_local_alt | `bool` | | | |
|
||||
| mode_req_local_position | `bool` | | | |
|
||||
| mode_req_local_position_relaxed | `bool` | | | |
|
||||
| mode_req_global_position | `bool` | | | |
|
||||
| mode_req_mission | `bool` | | | |
|
||||
| mode_req_home_position | `bool` | | | |
|
||||
| mode_req_prevent_arming | `bool` | | | |
|
||||
| mode_req_manual_control | `bool` | | | |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0 | |
|
||||
| <a href="#HEALTH_COMPONENT_INDEX_NONE"></a> HEALTH_COMPONENT_INDEX_NONE | `uint8` | 0 | |
|
||||
| <a href="#ORB_QUEUE_LENGTH"></a> ORB_QUEUE_LENGTH | `uint8` | 4 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/ArmingCheckReplyV0.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint32 MESSAGE_VERSION = 0
|
||||
@@ -37,5 +81,6 @@ bool mode_req_manual_control
|
||||
|
||||
|
||||
uint8 ORB_QUEUE_LENGTH = 4
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,10 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ArmingCheckRequest (повідомлення UORB)
|
||||
|
||||
Arming check request
|
||||
Arming check request.
|
||||
|
||||
Broadcast message to request arming checks be reported by all registered components, such as external ROS 2 navigation modes.
|
||||
All registered components should respond with an ArmingCheckReply message that indicates their current mode requirements, and any arming failure information.
|
||||
@@ -9,7 +13,28 @@ The request is sent regularly, even while armed, so that the FMU always knows th
|
||||
The reply will include the published request_id, allowing correlation of all arming check information for a particular request.
|
||||
The reply will also include the registration_id for each external component, provided to it during the registration process (RegisterExtComponentReply).
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/ArmingCheckRequest.msg)
|
||||
**TOPICS:** arming_checkrequest
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------------ | -------- | ---------------------------------------------------------------- | ---------- | ----------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| request_id | `uint8` | | | Id of this request. Allows correlation with associated ArmingCheckReply messages. |
|
||||
| valid_registrations_mask | `uint32` | | | Bitmask of valid registration ID's (the bit is also cleared if flagged as unresponsive) |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 1 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/ArmingCheckRequest.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Arming check request
|
||||
@@ -28,5 +53,6 @@ uint64 timestamp # [us] Time since system start
|
||||
uint8 request_id # [-] Id of this request. Allows correlation with associated ArmingCheckReply messages.
|
||||
|
||||
uint32 valid_registrations_mask # [-] Bitmask of valid registration ID's (the bit is also cleared if flagged as unresponsive)
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,3 +1,7 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ArmingCheckRequestV0 (UORB message)
|
||||
|
||||
Arming check request.
|
||||
@@ -9,7 +13,27 @@ The request is sent regularly, even while armed, so that the FMU always knows th
|
||||
The reply will include the published request_id, allowing correlation of all arming check information for a particular request.
|
||||
The reply will also include the registration_id for each external component, provided to it during the registration process (RegisterExtComponentReply).
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/ArmingCheckRequestV0.msg)
|
||||
**TOPICS:** arming_checkrequestv0
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | ----------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start. |
|
||||
| request_id | `uint8` | | | Id of this request. Allows correlation with associated ArmingCheckReply messages. |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/ArmingCheckRequestV0.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Arming check request.
|
||||
@@ -26,5 +50,6 @@ uint32 MESSAGE_VERSION = 0
|
||||
uint64 timestamp # [us] Time since system start.
|
||||
|
||||
uint8 request_id # Id of this request. Allows correlation with associated ArmingCheckReply messages.
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,13 +1,68 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# AutotuneAttitudeControlStatus (повідомлення UORB)
|
||||
|
||||
Autotune attitude control status
|
||||
Autotune attitude control status.
|
||||
|
||||
This message is published by the fw_autotune_attitude_control and mc_autotune_attitude_control modules when the user engages autotune,
|
||||
and is subscribed to by the respective attitude controllers to command rate setpoints.
|
||||
|
||||
The rate_sp field is consumed by the controllers, while the remaining fields (model coefficients, gains, filters, and autotune state) are used for logging and debugging.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/AutotuneAttitudeControlStatus.msg)
|
||||
**TOPICS:** autotune_attitudecontrol_status
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------ | ------------ | ---------------------------------------------------------------- | --------------- | -------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| coeff | `float32[5]` | | | Coefficients of the identified discrete-time model |
|
||||
| coeff_var | `float32[5]` | | | Coefficients' variance of the identified discrete-time model |
|
||||
| fitness | `float32` | | | Fitness of the parameter estimate |
|
||||
| innov | `float32` | rad/s | | Innovation (residual error between model and measured output) |
|
||||
| dt_model | `float32` | s | | Model sample time used for identification |
|
||||
| kc | `float32` | | | Proportional rate-loop gain (ideal form) |
|
||||
| ki | `float32` | | | Integral rate-loop gain (ideal form) |
|
||||
| kd | `float32` | | | Derivative rate-loop gain (ideal form) |
|
||||
| kff | `float32` | | | Feedforward rate-loop gain |
|
||||
| att_p | `float32` | | | Proportional attitude gain |
|
||||
| rate_sp | `float32[3]` | rad/s | | Rate setpoint commanded to the attitude controller. |
|
||||
| u_filt | `float32` | | | Filtered input signal (normalized torque setpoint) used in system identification. |
|
||||
| y_filt | `float32` | rad/s | | Filtered output signal (angular velocity) used in system identification. |
|
||||
| state | `uint8` | | [STATE](#STATE) | Current state of the autotune procedure. |
|
||||
|
||||
## Enums
|
||||
|
||||
### STATE {#STATE}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ---------------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ------------------------------------------------------------------------------------------- |
|
||||
| <a href="#STATE_IDLE"></a> STATE_IDLE | `uint8` | 0 | Idle (not running) |
|
||||
| <a href="#STATE_INIT"></a> STATE_INIT | `uint8` | 1 | Initialize filters and setup |
|
||||
| <a href="#STATE_ROLL_AMPLITUDE_DETECTION"></a> STATE_ROLL_AMPLITUDE_DETECTION | `uint8` | 2 | FW only: determine required excitation amplitude (roll) |
|
||||
| <a href="#STATE_ROLL"></a> STATE_ROLL | `uint8` | 3 | Roll-axis excitation and model identification |
|
||||
| <a href="#STATE_ROLL_PAUSE"></a> STATE_ROLL_PAUSE | `uint8` | 4 | Pause to return to level flight |
|
||||
| <a href="#STATE_PITCH_AMPLITUDE_DETECTION"></a> STATE_PITCH_AMPLITUDE_DETECTION | `uint8` | 5 | FW only: determine required excitation amplitude (pitch) |
|
||||
| <a href="#STATE_PITCH"></a> STATE_PITCH | `uint8` | 6 | Pitch-axis excitation and model identification |
|
||||
| <a href="#STATE_PITCH_PAUSE"></a> STATE_PITCH_PAUSE | `uint8` | 7 | Pause to return to level flight |
|
||||
| <a href="#STATE_YAW_AMPLITUDE_DETECTION"></a> STATE_YAW_AMPLITUDE_DETECTION | `uint8` | 8 | FW only: determine required excitation amplitude (yaw) |
|
||||
| <a href="#STATE_YAW"></a> STATE_YAW | `uint8` | 9 | Yaw-axis excitation and model identification |
|
||||
| <a href="#STATE_YAW_PAUSE"></a> STATE_YAW_PAUSE | `uint8` | 10 | Pause to return to level flight |
|
||||
| <a href="#STATE_VERIFICATION"></a> STATE_VERIFICATION | `uint8` | 11 | Verify model and candidate gains |
|
||||
| <a href="#STATE_APPLY"></a> STATE_APPLY | `uint8` | 12 | Apply gains |
|
||||
| <a href="#STATE_TEST"></a> STATE_TEST | `uint8` | 13 | Test gains in closed-loop |
|
||||
| <a href="#STATE_COMPLETE"></a> STATE_COMPLETE | `uint8` | 14 | Tuning completed successfully |
|
||||
| <a href="#STATE_FAIL"></a> STATE_FAIL | `uint8` | 15 | Tuning failed (model invalid or controller unstable) |
|
||||
| <a href="#STATE_WAIT_FOR_DISARM"></a> STATE_WAIT_FOR_DISARM | `uint8` | 16 | Waiting for disarm before finalizing |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/AutotuneAttitudeControlStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Autotune attitude control status
|
||||
@@ -55,5 +110,6 @@ uint8 STATE_TEST = 13 # Test gains in closed-loop
|
||||
uint8 STATE_COMPLETE = 14 # Tuning completed successfully
|
||||
uint8 STATE_FAIL = 15 # Tuning failed (model invalid or controller unstable)
|
||||
uint8 STATE_WAIT_FOR_DISARM = 16 # Waiting for disarm before finalizing
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,11 +1,30 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# BatteryInfo (UORB message)
|
||||
|
||||
Battery information
|
||||
Battery information.
|
||||
|
||||
Static or near-invariant battery information.
|
||||
Should be streamed at low rate.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/BatteryInfo.msg)
|
||||
**TOPICS:** battery_info
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ---------------------------------- | ---------- | ---------------------------------------------------------------- | ---------- | ----------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| id | `uint8` | | | Must match the id in the battery_status message for the same battery |
|
||||
| serial_number | `char[32]` | | | Serial number of the battery pack in ASCII characters, 0 terminated (Invalid: 0 All bytes) |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/BatteryInfo.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Battery information
|
||||
@@ -17,5 +36,6 @@ uint64 timestamp # [us] Time since system start
|
||||
|
||||
uint8 id # Must match the id in the battery_status message for the same battery
|
||||
char[32] serial_number # [@invalid 0 All bytes] Serial number of the battery pack in ASCII characters, 0 terminated
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,12 +1,117 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# BatteryStatus (повідомлення UORB)
|
||||
|
||||
Battery status
|
||||
Battery status.
|
||||
|
||||
Battery status information for up to 3 battery instances.
|
||||
These are populated from power module and smart battery device drivers, and one battery updated from MAVLink.
|
||||
Battery instance information is also logged and streamed in MAVLink telemetry.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/BatteryStatus.msg)
|
||||
**TOPICS:** battery_status
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| -------------------------------------------------------------------------------------- | ------------- | ---------------------------------------------------------------- | ----------------------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| connected | `bool` | | | Whether or not a battery is connected. For power modules this is based on a voltage threshold. |
|
||||
| voltage_v | `float32` | V | | Battery voltage (Invalid: 0) |
|
||||
| current_a | `float32` | A | | Battery current (Invalid: -1) |
|
||||
| current_average_a | `float32` | A | | Battery current average (for FW average in level flight) (Invalid: -1) |
|
||||
| discharged_mah | `float32` | mAh | | Discharged amount (Invalid: -1) |
|
||||
| remaining | `float32` | | [0 : 1] | Remaining capacity (Invalid: -1) |
|
||||
| scale | `float32` | | [1 : -] | Scaling factor to compensate for lower actuation power caused by voltage sag (Invalid: -1) |
|
||||
| time_remaining_s | `float32` | s | | Predicted time remaining until battery is empty under previous averaged load (Invalid: NaN) |
|
||||
| temperature | `float32` | °C | | Temperature of the battery (Invalid: NaN) |
|
||||
| cell_count | `uint8` | | | Number of cells (Invalid: 0) |
|
||||
| source | `uint8` | | [SOURCE](#SOURCE) | Battery source |
|
||||
| priority | `uint8` | | | Zero based priority is the connection on the Power Controller V1..Vn AKA BrickN-1 |
|
||||
| capacity | `uint16` | mAh | | Capacity of the battery when fully charged |
|
||||
| cycle_count | `uint16` | | | Number of discharge cycles the battery has experienced |
|
||||
| average_time_to_empty | `uint16` | minutes | | Predicted remaining battery capacity based on the average rate of discharge |
|
||||
| manufacture_date | `uint16` | | | Manufacture date, part of serial number of the battery pack. Formatted as: Day + Month×32 + (Year–1980)×512 |
|
||||
| state_of_health | `uint16` | % | [0 : 100] | State of health. FullChargeCapacity/DesignCapacity |
|
||||
| max_error | `uint16` | % | [1 : 100] | Max error, expected margin of error in the state-of-charge calculation |
|
||||
| id | `uint8` | | | ID number of a battery. Should be unique and consistent for the lifetime of a vehicle. 1-indexed |
|
||||
| interface_error | `uint16` | | | Interface error counter |
|
||||
| voltage_cell_v | `float32[14]` | V | | Battery individual cell voltages (Invalid: 0) |
|
||||
| max_cell_voltage_delta | `float32` | V | | Max difference between individual cell voltages |
|
||||
| is_powering_off | `bool` | | | Power off event imminent indication, false if unknown |
|
||||
| is_required | `bool` | | | Set if the battery is explicitly required before arming |
|
||||
| warning | `uint8` | | [WARNING](#WARNING)[STATE](#STATE) | Current battery warning |
|
||||
| faults | `uint16` | | [FAULT](#FAULT) | Smart battery supply status/fault flags (bitmask) for health indication |
|
||||
| full_charge_capacity_wh | `float32` | Wh | | Compensated battery capacity |
|
||||
| remaining_capacity_wh | `float32` | Wh | | Compensated battery capacity remaining |
|
||||
| over_discharge_count | `uint16` | | | Number of battery overdischarge |
|
||||
| nominal_voltage | `float32` | V | | Nominal voltage of the battery pack |
|
||||
| internal_resistance_estimate | `float32` | Ohm | | Internal resistance per cell estimate |
|
||||
| ocv_estimate | `float32` | V | | Open circuit voltage estimate |
|
||||
| ocv_estimate_filtered | `float32` | V | | Filtered open circuit voltage estimate |
|
||||
| volt_based_soc_estimate | `float32` | | [0 : 1] | Normalized volt based state of charge estimate |
|
||||
| voltage_prediction | `float32` | V | | Predicted voltage |
|
||||
| prediction_error | `float32` | V | | Prediction error |
|
||||
| estimation_covariance_norm | `float32` | | | Norm of the covariance matrix |
|
||||
|
||||
## Enums
|
||||
|
||||
### SOURCE {#SOURCE}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------------- | ------- | -------- | ----------------------------------------------------------------- |
|
||||
| <a href="#SOURCE_POWER_MODULE"></a> SOURCE_POWER_MODULE | `uint8` | 0 | Power module (analog ADC or I2C power monitor) |
|
||||
| <a href="#SOURCE_EXTERNAL"></a> SOURCE_EXTERNAL | `uint8` | 1 | External (MAVLink, CAN, or external driver) |
|
||||
| <a href="#SOURCE_ESCS"></a> SOURCE_ESCS | `uint8` | 2 | ESCs (via ESC telemetry) |
|
||||
|
||||
### WARNING {#WARNING}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------ | ------- | -------- | -------------------------------------------- |
|
||||
| <a href="#WARNING_NONE"></a> WARNING_NONE | `uint8` | 0 | No battery low voltage warning active |
|
||||
| <a href="#WARNING_LOW"></a> WARNING_LOW | `uint8` | 1 | Low voltage warning |
|
||||
| <a href="#WARNING_CRITICAL"></a> WARNING_CRITICAL | `uint8` | 2 | Critical voltage, return / abort immediately |
|
||||
| <a href="#WARNING_EMERGENCY"></a> WARNING_EMERGENCY | `uint8` | 3 | Immediate landing required |
|
||||
| <a href="#WARNING_FAILED"></a> WARNING_FAILED | `uint8` | 4 | Battery has failed completely |
|
||||
|
||||
### STATE {#STATE}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------- | ------- | -------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
|
||||
| <a href="#STATE_UNHEALTHY"></a> STATE_UNHEALTHY | `uint8` | 6 | Battery is diagnosed to be defective or an error occurred, usage is discouraged / prohibited. Possible causes (faults) are listed in faults field |
|
||||
| <a href="#STATE_CHARGING"></a> STATE_CHARGING | `uint8` | 7 | Battery is charging |
|
||||
|
||||
### FAULT {#FAULT}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ---------------------------------------------------------------------------------------------------------------------- | ------- | -------- | --------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| <a href="#FAULT_DEEP_DISCHARGE"></a> FAULT_DEEP_DISCHARGE | `uint8` | 0 | Battery has deep discharged |
|
||||
| <a href="#FAULT_SPIKES"></a> FAULT_SPIKES | `uint8` | 1 | Voltage spikes |
|
||||
| <a href="#FAULT_CELL_FAIL"></a> FAULT_CELL_FAIL | `uint8` | 2 | One or more cells have failed |
|
||||
| <a href="#FAULT_OVER_CURRENT"></a> FAULT_OVER_CURRENT | `uint8` | 3 | Over-current |
|
||||
| <a href="#FAULT_OVER_TEMPERATURE"></a> FAULT_OVER_TEMPERATURE | `uint8` | 4 | Over-temperature |
|
||||
| <a href="#FAULT_UNDER_TEMPERATURE"></a> FAULT_UNDER_TEMPERATURE | `uint8` | 5 | Under-temperature fault |
|
||||
| <a href="#FAULT_INCOMPATIBLE_VOLTAGE"></a> FAULT_INCOMPATIBLE_VOLTAGE | `uint8` | 6 | Vehicle voltage is not compatible with this battery (batteries on same power rail should have similar voltage) |
|
||||
| <a href="#FAULT_INCOMPATIBLE_FIRMWARE"></a> FAULT_INCOMPATIBLE_FIRMWARE | `uint8` | 7 | Battery firmware is not compatible with current autopilot firmware |
|
||||
| <a href="#FAULT_INCOMPATIBLE_MODEL"></a> FAULT_INCOMPATIBLE_MODEL | `uint8` | 8 | Battery model is not supported by the system |
|
||||
| <a href="#FAULT_HARDWARE_FAILURE"></a> FAULT_HARDWARE_FAILURE | `uint8` | 9 | Hardware problem |
|
||||
| <a href="#FAULT_FAILED_TO_ARM"></a> FAULT_FAILED_TO_ARM | `uint8` | 10 | Battery had a problem while arming |
|
||||
| <a href="#FAULT_COUNT"></a> FAULT_COUNT | `uint8` | 11 | Counter. Keep this as last element |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 1 | |
|
||||
| <a href="#MAX_INSTANCES"></a> MAX_INSTANCES | `uint8` | 3 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/BatteryStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Battery status
|
||||
@@ -88,5 +193,6 @@ float32 volt_based_soc_estimate # [-] [@range 0, 1] Normalized volt based
|
||||
float32 voltage_prediction # [V] Predicted voltage
|
||||
float32 prediction_error # [V] Prediction error
|
||||
float32 estimation_covariance_norm # [-] Norm of the covariance matrix
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,12 +1,118 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# BatteryStatusV0 (UORB message)
|
||||
|
||||
Battery status
|
||||
Battery status.
|
||||
|
||||
Battery status information for up to 4 battery instances.
|
||||
These are populated from power module and smart battery device drivers, and one battery updated from MAVLink.
|
||||
Battery instance information is also logged and streamed in MAVLink telemetry.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/BatteryStatusV0.msg)
|
||||
**TOPICS:** battery_statusv0
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| -------------------------------------------------------------------------------------- | ------------- | ---------------------------------------------------------------- | ----------------------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| connected | `bool` | | | Whether or not a battery is connected. For power modules this is based on a voltage threshold. |
|
||||
| voltage_v | `float32` | V | | Battery voltage (Invalid: 0) |
|
||||
| current_a | `float32` | A | | Battery current (Invalid: -1) |
|
||||
| current_average_a | `float32` | A | | Battery current average (for FW average in level flight) (Invalid: -1) |
|
||||
| discharged_mah | `float32` | mAh | | Discharged amount (Invalid: -1) |
|
||||
| remaining | `float32` | | [0 : 1] | Remaining capacity (Invalid: -1) |
|
||||
| scale | `float32` | | [1 : -] | Scaling factor to compensate for lower actuation power caused by voltage sag (Invalid: -1) |
|
||||
| time_remaining_s | `float32` | s | | Predicted time remaining until battery is empty under previous averaged load (Invalid: NaN) |
|
||||
| temperature | `float32` | °C | | Temperature of the battery (Invalid: NaN) |
|
||||
| cell_count | `uint8` | | | Number of cells (Invalid: 0) |
|
||||
| source | `uint8` | | [SOURCE](#SOURCE) | Battery source |
|
||||
| priority | `uint8` | | | Zero based priority is the connection on the Power Controller V1..Vn AKA BrickN-1 |
|
||||
| capacity | `uint16` | mAh | | Capacity of the battery when fully charged |
|
||||
| cycle_count | `uint16` | | | Number of discharge cycles the battery has experienced |
|
||||
| average_time_to_empty | `uint16` | minutes | | Predicted remaining battery capacity based on the average rate of discharge |
|
||||
| serial_number | `uint16` | | | Serial number of the battery pack |
|
||||
| manufacture_date | `uint16` | | | Manufacture date, part of serial number of the battery pack. Formatted as: Day + Month×32 + (Year–1980)×512 |
|
||||
| state_of_health | `uint16` | % | [0 : 100] | State of health. FullChargeCapacity/DesignCapacity |
|
||||
| max_error | `uint16` | % | [1 : 100] | Max error, expected margin of error in the state-of-charge calculation |
|
||||
| id | `uint8` | | | ID number of a battery. Should be unique and consistent for the lifetime of a vehicle. 1-indexed |
|
||||
| interface_error | `uint16` | | | Interface error counter |
|
||||
| voltage_cell_v | `float32[14]` | V | | Battery individual cell voltages (Invalid: 0) |
|
||||
| max_cell_voltage_delta | `float32` | | | Max difference between individual cell voltages |
|
||||
| is_powering_off | `bool` | | | Power off event imminent indication, false if unknown |
|
||||
| is_required | `bool` | | | Set if the battery is explicitly required before arming |
|
||||
| warning | `uint8` | | [WARNING](#WARNING)[STATE](#STATE) | Current battery warning |
|
||||
| faults | `uint16` | | [FAULT](#FAULT) | Smart battery supply status/fault flags (bitmask) for health indication |
|
||||
| full_charge_capacity_wh | `float32` | Wh | | Compensated battery capacity |
|
||||
| remaining_capacity_wh | `float32` | Wh | | Compensated battery capacity remaining |
|
||||
| over_discharge_count | `uint16` | | | Number of battery overdischarge |
|
||||
| nominal_voltage | `float32` | V | | Nominal voltage of the battery pack |
|
||||
| internal_resistance_estimate | `float32` | Ohm | | Internal resistance per cell estimate |
|
||||
| ocv_estimate | `float32` | V | | Open circuit voltage estimate |
|
||||
| ocv_estimate_filtered | `float32` | V | | Filtered open circuit voltage estimate |
|
||||
| volt_based_soc_estimate | `float32` | | [0 : 1] | Normalized volt based state of charge estimate |
|
||||
| voltage_prediction | `float32` | V | | Predicted voltage |
|
||||
| prediction_error | `float32` | V | | Prediction error |
|
||||
| estimation_covariance_norm | `float32` | | | Norm of the covariance matrix |
|
||||
|
||||
## Enums
|
||||
|
||||
### SOURCE {#SOURCE}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------------- | ------- | -------- | ----------------------------------------------------------------- |
|
||||
| <a href="#SOURCE_POWER_MODULE"></a> SOURCE_POWER_MODULE | `uint8` | 0 | Power module (analog ADC or I2C power monitor) |
|
||||
| <a href="#SOURCE_EXTERNAL"></a> SOURCE_EXTERNAL | `uint8` | 1 | External (MAVLink, CAN, or external driver) |
|
||||
| <a href="#SOURCE_ESCS"></a> SOURCE_ESCS | `uint8` | 2 | ESCs (via ESC telemetry) |
|
||||
|
||||
### WARNING {#WARNING}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------ | ------- | -------- | -------------------------------------------- |
|
||||
| <a href="#WARNING_NONE"></a> WARNING_NONE | `uint8` | 0 | No battery low voltage warning active |
|
||||
| <a href="#WARNING_LOW"></a> WARNING_LOW | `uint8` | 1 | Low voltage warning |
|
||||
| <a href="#WARNING_CRITICAL"></a> WARNING_CRITICAL | `uint8` | 2 | Critical voltage, return / abort immediately |
|
||||
| <a href="#WARNING_EMERGENCY"></a> WARNING_EMERGENCY | `uint8` | 3 | Immediate landing required |
|
||||
| <a href="#WARNING_FAILED"></a> WARNING_FAILED | `uint8` | 4 | Battery has failed completely |
|
||||
|
||||
### STATE {#STATE}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------- | ------- | -------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
|
||||
| <a href="#STATE_UNHEALTHY"></a> STATE_UNHEALTHY | `uint8` | 6 | Battery is diagnosed to be defective or an error occurred, usage is discouraged / prohibited. Possible causes (faults) are listed in faults field |
|
||||
| <a href="#STATE_CHARGING"></a> STATE_CHARGING | `uint8` | 7 | Battery is charging |
|
||||
|
||||
### FAULT {#FAULT}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ---------------------------------------------------------------------------------------------------------------------- | ------- | -------- | --------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| <a href="#FAULT_DEEP_DISCHARGE"></a> FAULT_DEEP_DISCHARGE | `uint8` | 0 | Battery has deep discharged |
|
||||
| <a href="#FAULT_SPIKES"></a> FAULT_SPIKES | `uint8` | 1 | Voltage spikes |
|
||||
| <a href="#FAULT_CELL_FAIL"></a> FAULT_CELL_FAIL | `uint8` | 2 | One or more cells have failed |
|
||||
| <a href="#FAULT_OVER_CURRENT"></a> FAULT_OVER_CURRENT | `uint8` | 3 | Over-current |
|
||||
| <a href="#FAULT_OVER_TEMPERATURE"></a> FAULT_OVER_TEMPERATURE | `uint8` | 4 | Over-temperature |
|
||||
| <a href="#FAULT_UNDER_TEMPERATURE"></a> FAULT_UNDER_TEMPERATURE | `uint8` | 5 | Under-temperature fault |
|
||||
| <a href="#FAULT_INCOMPATIBLE_VOLTAGE"></a> FAULT_INCOMPATIBLE_VOLTAGE | `uint8` | 6 | Vehicle voltage is not compatible with this battery (batteries on same power rail should have similar voltage) |
|
||||
| <a href="#FAULT_INCOMPATIBLE_FIRMWARE"></a> FAULT_INCOMPATIBLE_FIRMWARE | `uint8` | 7 | Battery firmware is not compatible with current autopilot firmware |
|
||||
| <a href="#FAULT_INCOMPATIBLE_MODEL"></a> FAULT_INCOMPATIBLE_MODEL | `uint8` | 8 | Battery model is not supported by the system |
|
||||
| <a href="#FAULT_HARDWARE_FAILURE"></a> FAULT_HARDWARE_FAILURE | `uint8` | 9 | Hardware problem |
|
||||
| <a href="#FAULT_FAILED_TO_ARM"></a> FAULT_FAILED_TO_ARM | `uint8` | 10 | Battery had a problem while arming |
|
||||
| <a href="#FAULT_COUNT"></a> FAULT_COUNT | `uint8` | 11 | Counter. Keep this as last element |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0 | |
|
||||
| <a href="#MAX_INSTANCES"></a> MAX_INSTANCES | `uint8` | 4 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/BatteryStatusV0.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Battery status
|
||||
@@ -88,5 +194,6 @@ float32 volt_based_soc_estimate # [@range 0, 1] Normalized volt based state of c
|
||||
float32 voltage_prediction # [V] Predicted voltage
|
||||
float32 prediction_error # [V] Prediction error
|
||||
float32 estimation_covariance_norm # Norm of the covariance matrix
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,30 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ButtonEvent (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ButtonEvent.msg)
|
||||
**TOPICS:** button_event safety_button
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| --------- | -------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| triggered | `bool` | | | Set to true if the event is triggered |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------- | ------- | -------- | ---- |
|
||||
| <a href="#ORB_QUEUE_LENGTH"></a> ORB_QUEUE_LENGTH | `uint8` | 2 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ButtonEvent.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -9,5 +33,6 @@ bool triggered # Set to true if the event is triggered
|
||||
# TOPICS button_event safety_button
|
||||
|
||||
uint8 ORB_QUEUE_LENGTH = 2
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,31 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# CameraCapture (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CameraCapture.msg)
|
||||
**TOPICS:** camera_capture
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------ | ------------ | ---------------------------------------------------------------- | ---------- | -------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_utc | `uint64` | | | Capture time in UTC / GPS time |
|
||||
| seq | `uint32` | | | Image sequence number |
|
||||
| lat | `float64` | | | Latitude in degrees (WGS84) |
|
||||
| lon | `float64` | | | Longitude in degrees (WGS84) |
|
||||
| alt | `float32` | | | Altitude (AMSL) |
|
||||
| ground_distance | `float32` | | | Altitude above ground (meters) |
|
||||
| q | `float32[4]` | | | Attitude of the camera relative to NED earth-fixed frame when using a gimbal, otherwise vehicle attitude |
|
||||
| result | `int8` | | | 1 for success, 0 for failure, -1 if camera does not provide feedback |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CameraCapture.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -12,5 +37,6 @@ float32 alt # Altitude (AMSL)
|
||||
float32 ground_distance # Altitude above ground (meters)
|
||||
float32[4] q # Attitude of the camera relative to NED earth-fixed frame when using a gimbal, otherwise vehicle attitude
|
||||
int8 result # 1 for success, 0 for failure, -1 if camera does not provide feedback
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,11 +1,31 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# CameraStatus (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CameraStatus.msg)
|
||||
**TOPICS:** camera_status
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| -------------------------------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| active_sys_id | `uint8` | | | mavlink system id of the currently active camera |
|
||||
| active_comp_id | `uint8` | | | mavlink component id of currently active camera |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CameraStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
|
||||
uint8 active_sys_id # mavlink system id of the currently active camera
|
||||
uint8 active_comp_id # mavlink component id of currently active camera
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,32 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# CameraTrigger (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CameraTrigger.msg)
|
||||
**TOPICS:** camera_trigger
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ---------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_utc | `uint64` | | | UTC timestamp |
|
||||
| seq | `uint32` | | | Image sequence number |
|
||||
| feedback | `bool` | | | Trigger feedback from camera |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#ORB_QUEUE_LENGTH"></a> ORB_QUEUE_LENGTH | `uint32` | 2 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CameraTrigger.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -10,5 +36,6 @@ uint32 seq # Image sequence number
|
||||
bool feedback # Trigger feedback from camera
|
||||
|
||||
uint32 ORB_QUEUE_LENGTH = 2
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,27 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# CanInterfaceStatus (повідомлення UORB)
|
||||
|
||||
[вихідний файл](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CanInterfaceStatus.msg)
|
||||
**TOPICS:** can_interfacestatus
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------ | -------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| інтерфейс | `uint8` | | | |
|
||||
| io_errors | `uint64` | | | |
|
||||
| frames_tx | `uint64` | | | |
|
||||
| frames_rx | `uint64` | | | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CanInterfaceStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -9,5 +30,6 @@ uint8 interface
|
||||
uint64 io_errors
|
||||
uint64 frames_tx
|
||||
uint64 frames_rx
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,10 +1,73 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# CellularStatus (повідомлення UORB)
|
||||
|
||||
Cellular status
|
||||
Cellular status.
|
||||
|
||||
This is currently used only for logging cell status from MAVLink.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CellularStatus.msg)
|
||||
**TOPICS:** cellular_status
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ----------------------------------- | -------- | ---------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------------------- | ------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| status | `uint16` | | [STATUS_FLAG](#STATUS_FLAG) | Status bitmap |
|
||||
| failure_reason | `uint8` | | [FAILURE_REASON](#FAILURE_REASON) | Failure reason |
|
||||
| type | `uint8` | | [CELLULAR_NETWORK_RADIO_TYPE](#CELLULAR_NETWORK_RADIO_TYPE) | Cellular network radio type |
|
||||
| quality | `uint8` | dBm | | Cellular network RSSI/RSRP, absolute value |
|
||||
| mcc | `uint16` | | | Mobile country code (Invalid: UINT16_MAX) |
|
||||
| mnc | `uint16` | | | Mobile network code (Invalid: UINT16_MAX) |
|
||||
| lac | `uint16` | | | Location area code (Invalid: 0) |
|
||||
|
||||
## Enums
|
||||
|
||||
### STATUS_FLAG {#STATUS_FLAG}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------------------------- | -------- | -------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| <a href="#STATUS_FLAG_UNKNOWN"></a> STATUS_FLAG_UNKNOWN | `uint16` | 1 | State unknown or not reportable |
|
||||
| <a href="#STATUS_FLAG_FAILED"></a> STATUS_FLAG_FAILED | `uint16` | 2 | Modem is unusable |
|
||||
| <a href="#STATUS_FLAG_INITIALIZING"></a> STATUS_FLAG_INITIALIZING | `uint16` | 4 | Modem is being initialized |
|
||||
| <a href="#STATUS_FLAG_LOCKED"></a> STATUS_FLAG_LOCKED | `uint16` | 8 | Modem is locked |
|
||||
| <a href="#STATUS_FLAG_DISABLED"></a> STATUS_FLAG_DISABLED | `uint16` | 16 | Modem is not enabled and is powered down |
|
||||
| <a href="#STATUS_FLAG_DISABLING"></a> STATUS_FLAG_DISABLING | `uint16` | 32 | Modem is currently transitioning to the STATUS_FLAG_DISABLED state |
|
||||
| <a href="#STATUS_FLAG_ENABLING"></a> STATUS_FLAG_ENABLING | `uint16` | 64 | Modem is currently transitioning to the STATUS_FLAG_ENABLED state |
|
||||
| <a href="#STATUS_FLAG_ENABLED"></a> STATUS_FLAG_ENABLED | `uint16` | 128 | Modem is enabled and powered on but not registered with a network provider and not available for data connections |
|
||||
| <a href="#STATUS_FLAG_SEARCHING"></a> STATUS_FLAG_SEARCHING | `uint16` | 256 | Modem is searching for a network provider to register |
|
||||
| <a href="#STATUS_FLAG_REGISTERED"></a> STATUS_FLAG_REGISTERED | `uint16` | 512 | Modem is registered with a network provider, and data connections and messaging may be available for use |
|
||||
| <a href="#STATUS_FLAG_DISCONNECTING"></a> STATUS_FLAG_DISCONNECTING | `uint16` | 1024 | Modem is disconnecting and deactivating the last active packet data bearer. This state will not be entered if more than one packet data bearer is active and one of the active bearers is deactivated |
|
||||
| <a href="#STATUS_FLAG_CONNECTING"></a> STATUS_FLAG_CONNECTING | `uint16` | 2048 | Modem is activating and connecting the first packet data bearer. Subsequent bearer activations when another bearer is already active do not cause this state to be entered |
|
||||
| <a href="#STATUS_FLAG_CONNECTED"></a> STATUS_FLAG_CONNECTED | `uint16` | 4096 | One or more packet data bearers is active and connected |
|
||||
|
||||
### FAILURE_REASON {#FAILURE_REASON}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------------------------------------------------ | ------- | -------- | ----------------------------------------------- |
|
||||
| <a href="#FAILURE_REASON_NONE"></a> FAILURE_REASON_NONE | `uint8` | 0 | No error |
|
||||
| <a href="#FAILURE_REASON_UNKNOWN"></a> FAILURE_REASON_UNKNOWN | `uint8` | 1 | Error state is unknown |
|
||||
| <a href="#FAILURE_REASON_SIM_MISSING"></a> FAILURE_REASON_SIM_MISSING | `uint8` | 2 | SIM is required for the modem but missing |
|
||||
| <a href="#FAILURE_REASON_SIM_ERROR"></a> FAILURE_REASON_SIM_ERROR | `uint8` | 3 | SIM is available, but not usable for connection |
|
||||
|
||||
### CELLULAR_NETWORK_RADIO_TYPE {#CELLULAR_NETWORK_RADIO_TYPE}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ----- |
|
||||
| <a href="#CELLULAR_NETWORK_RADIO_TYPE_NONE"></a> CELLULAR_NETWORK_RADIO_TYPE_NONE | `uint8` | 0 | None |
|
||||
| <a href="#CELLULAR_NETWORK_RADIO_TYPE_GSM"></a> CELLULAR_NETWORK_RADIO_TYPE_GSM | `uint8` | 1 | GSM |
|
||||
| <a href="#CELLULAR_NETWORK_RADIO_TYPE_CDMA"></a> CELLULAR_NETWORK_RADIO_TYPE_CDMA | `uint8` | 2 | CDMA |
|
||||
| <a href="#CELLULAR_NETWORK_RADIO_TYPE_WCDMA"></a> CELLULAR_NETWORK_RADIO_TYPE_WCDMA | `uint8` | 3 | WCDMA |
|
||||
| <a href="#CELLULAR_NETWORK_RADIO_TYPE_LTE"></a> CELLULAR_NETWORK_RADIO_TYPE_LTE | `uint8` | 4 | LTE |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CellularStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Cellular status
|
||||
@@ -45,5 +108,6 @@ uint8 quality # [dBm] Cellular network RSSI/RSRP, absolute value
|
||||
uint16 mcc # [@invalid UINT16_MAX] Mobile country code
|
||||
uint16 mnc # [@invalid UINT16_MAX] Mobile network code
|
||||
uint16 lac # [@invalid 0] Location area code
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,9 +1,27 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# CollisionConstraints (повідомлення UORB)
|
||||
|
||||
Обмеження локальної заданої точки в рамці NED
|
||||
встановлення чого-небудь на NaN означає, що обмеження не надано
|
||||
Local setpoint constraints in NED frame. setting something to NaN means that no limit is provided.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CollisionConstraints.msg)
|
||||
**TOPICS:** collision_constraints
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| -------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| original_setpoint | `float32[2]` | | | velocities demanded |
|
||||
| adapted_setpoint | `float32[2]` | | | velocities allowed |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/CollisionConstraints.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Local setpoint constraints in NED frame
|
||||
@@ -13,5 +31,6 @@ uint64 timestamp # time since system start (microseconds)
|
||||
|
||||
float32[2] original_setpoint # velocities demanded
|
||||
float32[2] adapted_setpoint # velocities allowed
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,8 +1,40 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ConfigOverrides (повідомлення UORB)
|
||||
|
||||
Конфігуровані перевизначення (зовнішніми) режимами або виконавцями режимів
|
||||
Configurable overrides by (external) modes or mode executors.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/ConfigOverrides.msg)
|
||||
**TOPICS:** config_overrides config_overrides_request
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ---------------------------------------------------------------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | ----------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| disable_auto_disarm | `bool` | | | Prevent the drone from automatically disarming after landing (if configured) |
|
||||
| defer_failsafes | `bool` | | | Defer all failsafes that can be deferred (until the flag is cleared) |
|
||||
| defer_failsafes_timeout_s | `int16` | | | Maximum time a failsafe can be deferred. 0 = system default, -1 = no timeout |
|
||||
| disable_auto_set_home | `bool` | | | Prevent the drone from automatically setting the home position on arm or takeoff |
|
||||
| source_type | `int8` | | | |
|
||||
| source_id | `uint8` | | | ID depending on source_type |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ---------------------------------------------------------------------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 1 | |
|
||||
| <a href="#SOURCE_TYPE_MODE"></a> SOURCE_TYPE_MODE | `int8` | 0 | |
|
||||
| <a href="#SOURCE_TYPE_MODE_EXECUTOR"></a> SOURCE_TYPE_MODE_EXECUTOR | `int8` | 1 | |
|
||||
| <a href="#ORB_QUEUE_LENGTH"></a> ORB_QUEUE_LENGTH | `uint8` | 4 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/ConfigOverrides.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Configurable overrides by (external) modes or mode executors
|
||||
@@ -26,5 +58,6 @@ uint8 source_id # ID depending on source_type
|
||||
uint8 ORB_QUEUE_LENGTH = 4
|
||||
|
||||
# TOPICS config_overrides config_overrides_request
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,8 +1,39 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ConfigOverridesV0 (UORB message)
|
||||
|
||||
Конфігуровані перевизначення (зовнішніми) режимами або виконавцями режимів
|
||||
Configurable overrides by (external) modes or mode executors.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/ConfigOverridesV0.msg)
|
||||
**TOPICS:** config_overrides config_overrides_request
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ---------------------------------------------------------------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | ----------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| disable_auto_disarm | `bool` | | | Prevent the drone from automatically disarming after landing (if configured) |
|
||||
| defer_failsafes | `bool` | | | Defer all failsafes that can be deferred (until the flag is cleared) |
|
||||
| defer_failsafes_timeout_s | `int16` | | | Maximum time a failsafe can be deferred. 0 = system default, -1 = no timeout |
|
||||
| source_type | `int8` | | | |
|
||||
| source_id | `uint8` | | | ID depending on source_type |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ---------------------------------------------------------------------------------------------------------------------------------- | -------- | -------- | ---- |
|
||||
| <a href="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0 | |
|
||||
| <a href="#SOURCE_TYPE_MODE"></a> SOURCE_TYPE_MODE | `int8` | 0 | |
|
||||
| <a href="#SOURCE_TYPE_MODE_EXECUTOR"></a> SOURCE_TYPE_MODE_EXECUTOR | `int8` | 1 | |
|
||||
| <a href="#ORB_QUEUE_LENGTH"></a> ORB_QUEUE_LENGTH | `uint8` | 4 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/ConfigOverridesV0.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Configurable overrides by (external) modes or mode executors
|
||||
@@ -26,5 +57,6 @@ uint8 source_id # ID depending on source_type
|
||||
uint8 ORB_QUEUE_LENGTH = 4
|
||||
|
||||
# TOPICS config_overrides config_overrides_request
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,40 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# ControlAllocatorStatus (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ControlAllocatorStatus.msg)
|
||||
**TOPICS:** control_allocatorstatus
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ----------------------------------------------------------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| torque_setpoint_achieved | `bool` | | | Boolean indicating whether the 3D torque setpoint was correctly allocated to actuators. 0 if not achieved, 1 if achieved. |
|
||||
| unallocated_torque | `float32[3]` | | | Unallocated torque. Equal to 0 if the setpoint was achieved. |
|
||||
| thrust_setpoint_achieved | `bool` | | | Boolean indicating whether the 3D thrust setpoint was correctly allocated to actuators. 0 if not achieved, 1 if achieved. |
|
||||
| unallocated_thrust | `float32[3]` | | | Unallocated thrust. Equal to 0 if the setpoint was achieved. |
|
||||
| actuator_saturation | `int8[16]` | | | Indicates actuator saturation status. |
|
||||
| handled_motor_failure_mask | `uint16` | | | Bitmask of failed motors that were removed from the allocation / effectiveness matrix. Not necessarily identical to the report from FailureDetector |
|
||||
| motor_stop_mask | `uint16` | | | Bitmaks of motors stopped by failure injection |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------------------------------------------------------ | ------ | -------- | ----------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| <a href="#ACTUATOR_SATURATION_OK"></a> ACTUATOR_SATURATION_OK | `int8` | 0 | The actuator is not saturated |
|
||||
| <a href="#ACTUATOR_SATURATION_UPPER_DYN"></a> ACTUATOR_SATURATION_UPPER_DYN | `int8` | 1 | The actuator is saturated (with a value <= the desired value) because it cannot increase its value faster |
|
||||
| <a href="#ACTUATOR_SATURATION_UPPER"></a> ACTUATOR_SATURATION_UPPER | `int8` | 2 | The actuator is saturated (with a value <= the desired value) because it has reached its maximum value |
|
||||
| <a href="#ACTUATOR_SATURATION_LOWER_DYN"></a> ACTUATOR_SATURATION_LOWER_DYN | `int8` | -1 | The actuator is saturated (with a value >= the desired value) because it cannot decrease its value faster |
|
||||
| <a href="#ACTUATOR_SATURATION_LOWER"></a> ACTUATOR_SATURATION_LOWER | `int8` | -2 | The actuator is saturated (with a value >= the desired value) because it has reached its minimum value |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/ControlAllocatorStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -25,5 +59,6 @@ int8[16] actuator_saturation # Indicates actuator saturation status.
|
||||
|
||||
uint16 handled_motor_failure_mask # Bitmask of failed motors that were removed from the allocation / effectiveness matrix. Not necessarily identical to the report from FailureDetector
|
||||
uint16 motor_stop_mask # Bitmaks of motors stopped by failure injection
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,10 +1,30 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# Cpuload (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/Cpuload.msg)
|
||||
**TOPICS:** cpuload
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------ | --------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| load | `float32` | | | processor load from 0 to 1 |
|
||||
| ram_usage | `float32` | | | RAM usage from 0 to 1 |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/Cpuload.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
float32 load # processor load from 0 to 1
|
||||
float32 ram_usage # RAM usage from 0 to 1
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,29 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DatamanRequest (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DatamanRequest.msg)
|
||||
**TOPICS:** dataman_request
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| --------------------------------- | ----------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| client_id | `uint8` | | | |
|
||||
| request_type | `uint8` | | | id/read/write/clear |
|
||||
| item | `uint8` | | | dm_item_t |
|
||||
| index | `uint32` | | | |
|
||||
| data | `uint8[56]` | | | |
|
||||
| data_length | `uint32` | | | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DatamanRequest.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -11,5 +34,6 @@ uint8 item # dm_item_t
|
||||
uint32 index
|
||||
uint8[56] data
|
||||
uint32 data_length
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,40 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DatamanResponse (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DatamanResponse.msg)
|
||||
**TOPICS:** dataman_response
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| --------------------------------- | ----------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| client_id | `uint8` | | | |
|
||||
| request_type | `uint8` | | | id/read/write/clear |
|
||||
| item | `uint8` | | | dm_item_t |
|
||||
| index | `uint32` | | | |
|
||||
| data | `uint8[56]` | | | |
|
||||
| status | `uint8` | | | |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ---- |
|
||||
| <a href="#STATUS_SUCCESS"></a> STATUS_SUCCESS | `uint8` | 0 | |
|
||||
| <a href="#STATUS_FAILURE_ID_ERR"></a> STATUS_FAILURE_ID_ERR | `uint8` | 1 | |
|
||||
| <a href="#STATUS_FAILURE_NO_DATA"></a> STATUS_FAILURE_NO_DATA | `uint8` | 2 | |
|
||||
| <a href="#STATUS_FAILURE_READ_FAILED"></a> STATUS_FAILURE_READ_FAILED | `uint8` | 3 | |
|
||||
| <a href="#STATUS_FAILURE_WRITE_FAILED"></a> STATUS_FAILURE_WRITE_FAILED | `uint8` | 4 | |
|
||||
| <a href="#STATUS_FAILURE_CLEAR_FAILED"></a> STATUS_FAILURE_CLEAR_FAILED | `uint8` | 5 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DatamanResponse.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -18,5 +52,6 @@ uint8 STATUS_FAILURE_READ_FAILED = 3
|
||||
uint8 STATUS_FAILURE_WRITE_FAILED = 4
|
||||
uint8 STATUS_FAILURE_CLEAR_FAILED = 5
|
||||
uint8 status
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,32 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DebugArray (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DebugArray.msg)
|
||||
**TOPICS:** debug_array
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| --------- | ------------- | ---------------------------------------------------------------- | ---------- | ------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| id | `uint16` | | | unique ID of debug array, used to discriminate between arrays |
|
||||
| name | `char[10]` | | | name of the debug array (max. 10 characters) |
|
||||
| data | `float32[58]` | | | data |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ---------------------------------------------------------- | ------- | -------- | ---- |
|
||||
| <a href="#ARRAY_SIZE"></a> ARRAY_SIZE | `uint8` | 58 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DebugArray.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint8 ARRAY_SIZE = 58
|
||||
@@ -8,5 +34,6 @@ uint64 timestamp # time since system start (microseconds)
|
||||
uint16 id # unique ID of debug array, used to discriminate between arrays
|
||||
char[10] name # name of the debug array (max. 10 characters)
|
||||
float32[58] data # data
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,10 +1,30 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DebugKeyValue (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DebugKeyValue.msg)
|
||||
**TOPICS:** debug_keyvalue
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| --------- | ---------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| key | `char[10]` | | | max. 10 characters as key / name |
|
||||
| value | `float32` | | | the value to send as debug output |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DebugKeyValue.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
char[10] key # max. 10 characters as key / name
|
||||
float32 value # the value to send as debug output
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,10 +1,30 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DebugValue (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DebugValue.msg)
|
||||
**TOPICS:** debug_value
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| --------- | --------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| ind | `int8` | | | index of debug variable |
|
||||
| value | `float32` | | | the value to send as debug output |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DebugValue.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
int8 ind # index of debug variable
|
||||
float32 value # the value to send as debug output
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,27 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DebugVect (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DebugVect.msg)
|
||||
**TOPICS:** debug_vect
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| --------- | ---------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| name | `char[10]` | | | max. 10 characters as key / name |
|
||||
| x | `float32` | | | x value |
|
||||
| y | `float32` | | | y value |
|
||||
| z | `float32` | | | z value |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DebugVect.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -8,5 +29,6 @@ char[10] name # max. 10 characters as key / name
|
||||
float32 x # x value
|
||||
float32 y # y value
|
||||
float32 z # z value
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,11 +1,58 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DeviceInformation (UORB message)
|
||||
|
||||
Device information
|
||||
Device information.
|
||||
|
||||
Can be used to uniquely associate a device_id from a sensor topic with a physical device using serial number.
|
||||
as well as tracking of the used firmware versions on the devices.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DeviceInformation.msg)
|
||||
**TOPICS:** device_information
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------- | ---------- | ---------------------------------------------------------------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| device_type | `uint8` | | [DEVICE_TYPE](#DEVICE_TYPE) | Type of the device. Matches MAVLink DEVICE_TYPE enum |
|
||||
| vendor_name | `char[32]` | | | Name of the device vendor |
|
||||
| model_name | `char[32]` | | | Name of the device model |
|
||||
| `uint32` | | | Unique device ID for the sensor. Does not change between power cycles. (Invalid: 0 if not available) | |
|
||||
| firmware_version | `char[24]` | | | Firmware version. (Invalid: empty if not available) |
|
||||
| hardware_version | `char[24]` | | | Hardware version. (Invalid: empty if not available) |
|
||||
| serial_number | `char[33]` | | | Device serial number or unique identifier. (Invalid: empty if not available) |
|
||||
|
||||
## Enums
|
||||
|
||||
### DEVICE_TYPE {#DEVICE_TYPE}
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ---------------------- |
|
||||
| <a href="#DEVICE_TYPE_GENERIC"></a> DEVICE_TYPE_GENERIC | `uint8` | 0 | Generic/unknown sensor |
|
||||
| <a href="#DEVICE_TYPE_AIRSPEED"></a> DEVICE_TYPE_AIRSPEED | `uint8` | 1 | Датчик швидкості |
|
||||
| <a href="#DEVICE_TYPE_ESC"></a> DEVICE_TYPE_ESC | `uint8` | 2 | ESC |
|
||||
| <a href="#DEVICE_TYPE_SERVO"></a> DEVICE_TYPE_SERVO | `uint8` | 3 | Servo |
|
||||
| <a href="#DEVICE_TYPE_GPS"></a> DEVICE_TYPE_GPS | `uint8` | 4 | GPS |
|
||||
| <a href="#DEVICE_TYPE_MAGNETOMETER"></a> DEVICE_TYPE_MAGNETOMETER | `uint8` | 5 | Магнітометр |
|
||||
| <a href="#DEVICE_TYPE_PARACHUTE"></a> DEVICE_TYPE_PARACHUTE | `uint8` | 6 | Парашут |
|
||||
| <a href="#DEVICE_TYPE_RANGEFINDER"></a> DEVICE_TYPE_RANGEFINDER | `uint8` | 7 | Rangefinder |
|
||||
| <a href="#DEVICE_TYPE_WINCH"></a> DEVICE_TYPE_WINCH | `uint8` | 8 | Winch |
|
||||
| <a href="#DEVICE_TYPE_BAROMETER"></a> DEVICE_TYPE_BAROMETER | `uint8` | 9 | Барометр |
|
||||
| <a href="#DEVICE_TYPE_OPTICAL_FLOW"></a> DEVICE_TYPE_OPTICAL_FLOW | `uint8` | 10 | Optical flow |
|
||||
| <a href="#DEVICE_TYPE_ACCELEROMETER"></a> DEVICE_TYPE_ACCELEROMETER | `uint8` | 11 | Accelerometer |
|
||||
| <a href="#DEVICE_TYPE_GYROSCOPE"></a> DEVICE_TYPE_GYROSCOPE | `uint8` | 12 | Gyroscope |
|
||||
| <a href="#DEVICE_TYPE_DIFFERENTIAL_PRESSURE"></a> DEVICE_TYPE_DIFFERENTIAL_PRESSURE | `uint8` | 13 | Differential pressure |
|
||||
| <a href="#DEVICE_TYPE_BATTERY"></a> DEVICE_TYPE_BATTERY | `uint8` | 14 | Battery |
|
||||
| <a href="#DEVICE_TYPE_HYGROMETER"></a> DEVICE_TYPE_HYGROMETER | `uint8` | 15 | Hygrometer |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DeviceInformation.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Device information
|
||||
@@ -41,5 +88,6 @@ uint32 device_id # [-] [@invalid 0 if not available] Unique device ID
|
||||
char[24] firmware_version # [-] [@invalid empty if not available] Firmware version.
|
||||
char[24] hardware_version # [-] [@invalid empty if not available] Hardware version.
|
||||
char[33] serial_number # [-] [@invalid empty if not available] Device serial number or unique identifier.
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,11 +1,33 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DifferentialPressure (повідомлення UORB)
|
||||
|
||||
Differential-pressure (airspeed) sensor
|
||||
Differential-pressure (airspeed) sensor.
|
||||
|
||||
This is populated by airspeed sensor drivers and used by the sensor module to calculate airspeed.
|
||||
The information is published in the `SCALED_PRESSURE_n` MAVLink messages (along with information from a corresponding `SensorBaro` instance).
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DifferentialPressure.msg)
|
||||
**TOPICS:** differential_pressure
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------------ | --------- | ---------------------------------------------------------------- | ---------- | ------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time of publication (since system start) |
|
||||
| timestamp_sample | `uint64` | us | | Time of raw data capture |
|
||||
| device_id | `uint32` | | | Unique device ID for the sensor that does not change between power cycles |
|
||||
| differential_pressure_pa | `float32` | Pa | | Differential pressure reading (may be negative) |
|
||||
| temperature | `float32` | degC | | Temperature (Invalid: NaN if unknown) |
|
||||
| error_count | `uint32` | | | Number of errors detected by driver |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DifferentialPressure.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# Differential-pressure (airspeed) sensor
|
||||
@@ -20,5 +42,6 @@ uint32 device_id # [-] Unique device ID for the sensor that doe
|
||||
float32 differential_pressure_pa # [Pa] Differential pressure reading (may be negative)
|
||||
float32 temperature # [degC] [@invalid NaN if unknown] Temperature
|
||||
uint32 error_count # [-] Number of errors detected by driver
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,8 +1,64 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DistanceSensor (повідомлення UORB)
|
||||
|
||||
Дані повідомлення DISTANCE_SENSOR
|
||||
DISTANCE_SENSOR message data.
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DistanceSensor.msg)
|
||||
**TOPICS:** distance_sensor
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| device_id | `uint32` | | | unique device ID for the sensor that does not change between power cycles |
|
||||
| min_distance | `float32` | | | Minimum distance the sensor can measure (in m) |
|
||||
| max_distance | `float32` | | | Maximum distance the sensor can measure (in m) |
|
||||
| current_distance | `float32` | | | Current distance reading (in m) |
|
||||
| variance | `float32` | | | Measurement variance (in m^2), 0 for unknown / invalid readings |
|
||||
| signal_quality | `int8` | | | Signal quality in percent (0...100%), where 0 = invalid signal, 100 = perfect signal, and -1 = unknown signal quality. |
|
||||
| type | `uint8` | | | Type from MAV_DISTANCE_SENSOR enum |
|
||||
| h_fov | `float32` | | | Sensor horizontal field of view (rad) |
|
||||
| v_fov | `float32` | | | Sensor vertical field of view (rad) |
|
||||
| q | `float32[4]` | | | Quaterion sensor orientation with respect to the vehicle body frame to specify the orientation ROTATION_CUSTOM |
|
||||
| orientation | `uint8` | | | Direction the sensor faces from MAV_SENSOR_ORIENTATION enum |
|
||||
| mode | `uint8` | | | |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ----------------------------------------------------------------------------------------------------------------- |
|
||||
| <a href="#MAV_DISTANCE_SENSOR_LASER"></a> MAV_DISTANCE_SENSOR_LASER | `uint8` | 0 | |
|
||||
| <a href="#MAV_DISTANCE_SENSOR_ULTRASOUND"></a> MAV_DISTANCE_SENSOR_ULTRASOUND | `uint8` | 1 | |
|
||||
| <a href="#MAV_DISTANCE_SENSOR_INFRARED"></a> MAV_DISTANCE_SENSOR_INFRARED | `uint8` | 2 | |
|
||||
| <a href="#MAV_DISTANCE_SENSOR_RADAR"></a> MAV_DISTANCE_SENSOR_RADAR | `uint8` | 3 | |
|
||||
| <a href="#ROTATION_YAW_0 "></a> ROTATION_YAW_0 | `uint8` | 0 | MAV_SENSOR_ROTATION_NONE |
|
||||
| <a href="#ROTATION_YAW_45 "></a> ROTATION_YAW_45 | `uint8` | 1 | MAV_SENSOR_ROTATION_YAW_45 |
|
||||
| <a href="#ROTATION_YAW_90 "></a> ROTATION_YAW_90 | `uint8` | 2 | MAV_SENSOR_ROTATION_YAW_90 |
|
||||
| <a href="#ROTATION_YAW_135 "></a> ROTATION_YAW_135 | `uint8` | 3 | MAV_SENSOR_ROTATION_YAW_135 |
|
||||
| <a href="#ROTATION_YAW_180 "></a> ROTATION_YAW_180 | `uint8` | 4 | MAV_SENSOR_ROTATION_YAW_180 |
|
||||
| <a href="#ROTATION_YAW_225 "></a> ROTATION_YAW_225 | `uint8` | 5 | MAV_SENSOR_ROTATION_YAW_225 |
|
||||
| <a href="#ROTATION_YAW_270 "></a> ROTATION_YAW_270 | `uint8` | 6 | MAV_SENSOR_ROTATION_YAW_270 |
|
||||
| <a href="#ROTATION_YAW_315 "></a> ROTATION_YAW_315 | `uint8` | 7 | MAV_SENSOR_ROTATION_YAW_315 |
|
||||
| <a href="#ROTATION_FORWARD_FACING "></a> ROTATION_FORWARD_FACING | `uint8` | 0 | MAV_SENSOR_ROTATION_NONE |
|
||||
| <a href="#ROTATION_RIGHT_FACING "></a> ROTATION_RIGHT_FACING | `uint8` | 2 | MAV_SENSOR_ROTATION_YAW_90 |
|
||||
| <a href="#ROTATION_BACKWARD_FACING "></a> ROTATION_BACKWARD_FACING | `uint8` | 4 | MAV_SENSOR_ROTATION_YAW_180 |
|
||||
| <a href="#ROTATION_LEFT_FACING "></a> ROTATION_LEFT_FACING | `uint8` | 6 | MAV_SENSOR_ROTATION_YAW_270 |
|
||||
| <a href="#ROTATION_UPWARD_FACING"></a> ROTATION_UPWARD_FACING | `uint8` | 24 | MAV_SENSOR_ROTATION_PITCH_90 |
|
||||
| <a href="#ROTATION_DOWNWARD_FACING"></a> ROTATION_DOWNWARD_FACING | `uint8` | 25 | MAV_SENSOR_ROTATION_PITCH_270 |
|
||||
| <a href="#ROTATION_CUSTOM"></a> ROTATION_CUSTOM | `uint8` | 100 | MAV_SENSOR_ROTATION_CUSTOM |
|
||||
| <a href="#MODE_UNKNOWN"></a> MODE_UNKNOWN | `uint8` | 0 | |
|
||||
| <a href="#MODE_ENABLED"></a> MODE_ENABLED | `uint8` | 1 | |
|
||||
| <a href="#MODE_DISABLED"></a> MODE_DISABLED | `uint8` | 2 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DistanceSensor.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# DISTANCE_SENSOR message data
|
||||
@@ -52,5 +108,6 @@ uint8 mode
|
||||
uint8 MODE_UNKNOWN = 0
|
||||
uint8 MODE_ENABLED = 1
|
||||
uint8 MODE_DISABLED = 2
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,31 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DistanceSensorModeChangeRequest (UORB message)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DistanceSensorModeChangeRequest.msg)
|
||||
**TOPICS:** distance_sensormode_changerequest
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| -------------------------------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| request_on_off | `uint8` | | | request to disable/enable the distance sensor |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------ | ------- | -------- | ---- |
|
||||
| <a href="#REQUEST_OFF"></a> REQUEST_OFF | `uint8` | 0 | |
|
||||
| <a href="#REQUEST_ON"></a> REQUEST_ON | `uint8` | 1 | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DistanceSensorModeChangeRequest.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -8,5 +33,6 @@ uint64 timestamp # time since system start (microseconds)
|
||||
uint8 request_on_off # request to disable/enable the distance sensor
|
||||
uint8 REQUEST_OFF = 0
|
||||
uint8 REQUEST_ON = 1
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,43 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# DronecanNodeStatus (UORB message)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DronecanNodeStatus.msg)
|
||||
**TOPICS:** dronecan_nodestatus
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------------------------------------ | -------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| node_id | `uint16` | | | The node ID which this data comes from |
|
||||
| uptime_sec | `uint32` | | | Node uptime |
|
||||
| health | `uint8` | | | |
|
||||
| mode | `uint8` | | | |
|
||||
| sub_mode | `uint8` | | | |
|
||||
| vendor_specific_status_code | `uint16` | | | |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| --------------------------------------------------------------------------------------------------- | ------- | -------- | ----------------------------------------------------------------------------------------------- |
|
||||
| <a href="#HEALTH_OK"></a> HEALTH_OK | `uint8` | 0 | The node is functioning properly. |
|
||||
| <a href="#HEALTH_WARNING"></a> HEALTH_WARNING | `uint8` | 1 | A critical parameter went out of range or the node encountered a minor failure. |
|
||||
| <a href="#HEALTH_ERROR"></a> HEALTH_ERROR | `uint8` | 2 | The node encountered a major failure. |
|
||||
| <a href="#HEALTH_CRITICAL"></a> HEALTH_CRITICAL | `uint8` | 3 | The node suffered a fatal malfunction. |
|
||||
| <a href="#MODE_OPERATIONAL"></a> MODE_OPERATIONAL | `uint8` | 0 | Normal operating mode. |
|
||||
| <a href="#MODE_INITIALIZATION"></a> MODE_INITIALIZATION | `uint8` | 1 | Initialization is in progress; this mode is entered immediately after startup. |
|
||||
| <a href="#MODE_MAINTENANCE"></a> MODE_MAINTENANCE | `uint8` | 2 | Наприклад, calibration, the bootloader is running, etc. |
|
||||
| <a href="#MODE_SOFTWARE_UPDATE"></a> MODE_SOFTWARE_UPDATE | `uint8` | 3 | New software/firmware is being loaded. |
|
||||
| <a href="#MODE_OFFLINE"></a> MODE_OFFLINE | `uint8` | 7 | The node is no longer available. |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/DronecanNodeStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -44,5 +81,6 @@ uint8 sub_mode
|
||||
# Optional, vendor-specific node status code, e.g. a fault code or a status bitmask.
|
||||
#
|
||||
uint16 vendor_specific_status_code
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,11 +1,38 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# Ekf2Timestamps (повідомлення UORB)
|
||||
|
||||
це повідомлення містить (відносні) відмітки часу введення датчиків, які використовує EKF2.
|
||||
Це може бути використано для відтворення.
|
||||
це повідомлення містить (відносні) відмітки часу введення датчиків, які використовує EKF2. Це може бути використано для відтворення.
|
||||
|
||||
поле мітки часу - це посилання на час ekf2 і відповідає мітці часу теми sensor_combined.
|
||||
**TOPICS:** ekf2_timestamps
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/Ekf2Timestamps.msg)
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------------------------------------------------------------ | -------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| airspeed_timestamp_rel | `int16` | | | |
|
||||
| airspeed_validated_timestamp_rel | `int16` | | | |
|
||||
| distance_sensor_timestamp_rel | `int16` | | | |
|
||||
| optical_flow_timestamp_rel | `int16` | | | |
|
||||
| vehicle_air_data_timestamp_rel | `int16` | | | |
|
||||
| vehicle_magnetometer_timestamp_rel | `int16` | | | |
|
||||
| visual_odometry_timestamp_rel | `int16` | | | |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| --------------------------------------------------------------------------------------------------------------- | ------- | -------- | ------------------------------------------------------------- |
|
||||
| <a href="#RELATIVE_TIMESTAMP_INVALID"></a> RELATIVE_TIMESTAMP_INVALID | `int16` | 32767 | (0x7fff) If one of the relative timestamps |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/Ekf2Timestamps.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
# this message contains the (relative) timestamps of the sensor inputs used by EKF2.
|
||||
@@ -32,5 +59,6 @@ int16 vehicle_magnetometer_timestamp_rel
|
||||
int16 visual_odometry_timestamp_rel
|
||||
|
||||
# Note: this is a high-rate logged topic, so it needs to be as small as possible
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,62 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EscReport (UORB повідомлення)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EscReport.msg)
|
||||
**TOPICS:** esc_report
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| -------------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | -------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| esc_errorcount | `uint32` | | | Number of reported errors by ESC - if supported |
|
||||
| esc_rpm | `int32` | | | Motor RPM, negative for reverse rotation [RPM] - if supported |
|
||||
| esc_voltage | `float32` | | | Voltage measured from current ESC [V] - if supported |
|
||||
| esc_current | `float32` | | | Current measured from current ESC [A] - if supported |
|
||||
| esc_temperature | `float32` | | | Temperature measured from current ESC [degC] - if supported |
|
||||
| esc_address | `uint8` | | | Address of current ESC (in most cases 1-8 / must be set by driver) |
|
||||
| esc_cmdcount | `uint8` | | | Counter of number of commands |
|
||||
| esc_state | `uint8` | | | State of ESC - depend on Vendor |
|
||||
| actuator_function | `uint8` | | | actuator output function (one of Motor1...MotorN) |
|
||||
| failures | `uint16` | | | Bitmask to indicate the internal ESC faults |
|
||||
| esc_power | `int8` | | | Applied power 0-100 in % (negative values reserved) |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR1"></a> ACTUATOR_FUNCTION_MOTOR1 | `uint8` | 101 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR2"></a> ACTUATOR_FUNCTION_MOTOR2 | `uint8` | 102 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR3"></a> ACTUATOR_FUNCTION_MOTOR3 | `uint8` | 103 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR4"></a> ACTUATOR_FUNCTION_MOTOR4 | `uint8` | 104 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR5"></a> ACTUATOR_FUNCTION_MOTOR5 | `uint8` | 105 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR6"></a> ACTUATOR_FUNCTION_MOTOR6 | `uint8` | 106 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR7"></a> ACTUATOR_FUNCTION_MOTOR7 | `uint8` | 107 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR8"></a> ACTUATOR_FUNCTION_MOTOR8 | `uint8` | 108 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR9"></a> ACTUATOR_FUNCTION_MOTOR9 | `uint8` | 109 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR10"></a> ACTUATOR_FUNCTION_MOTOR10 | `uint8` | 110 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR11"></a> ACTUATOR_FUNCTION_MOTOR11 | `uint8` | 111 | |
|
||||
| <a href="#ACTUATOR_FUNCTION_MOTOR12"></a> ACTUATOR_FUNCTION_MOTOR12 | `uint8` | 112 | |
|
||||
| <a href="#FAILURE_OVER_CURRENT"></a> FAILURE_OVER_CURRENT | `uint8` | 0 | (1 << 0) |
|
||||
| <a href="#FAILURE_OVER_VOLTAGE"></a> FAILURE_OVER_VOLTAGE | `uint8` | 1 | (1 << 1) |
|
||||
| <a href="#FAILURE_MOTOR_OVER_TEMPERATURE"></a> FAILURE_MOTOR_OVER_TEMPERATURE | `uint8` | 2 | (1 << 2) |
|
||||
| <a href="#FAILURE_OVER_RPM"></a> FAILURE_OVER_RPM | `uint8` | 3 | (1 << 3) |
|
||||
| <a href="#FAILURE_INCONSISTENT_CMD"></a> FAILURE_INCONSISTENT_CMD | `uint8` | 4 | (1 << 4) Set if ESC received an inconsistent command (i.e out of boundaries) |
|
||||
| <a href="#FAILURE_MOTOR_STUCK"></a> FAILURE_MOTOR_STUCK | `uint8` | 5 | (1 << 5) |
|
||||
| <a href="#FAILURE_GENERIC"></a> FAILURE_GENERIC | `uint8` | 6 | (1 << 6) |
|
||||
| <a href="#FAILURE_MOTOR_WARN_TEMPERATURE"></a> FAILURE_MOTOR_WARN_TEMPERATURE | `uint8` | 7 | (1 << 7) |
|
||||
| <a href="#FAILURE_WARN_ESC_TEMPERATURE"></a> FAILURE_WARN_ESC_TEMPERATURE | `uint8` | 8 | (1 << 8) |
|
||||
| <a href="#FAILURE_OVER_ESC_TEMPERATURE"></a> FAILURE_OVER_ESC_TEMPERATURE | `uint8` | 9 | (1 << 9) |
|
||||
| <a href="#ESC_FAILURE_COUNT"></a> ESC_FAILURE_COUNT | `uint8` | 10 | Counter - keep it as last element! |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EscReport.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -43,5 +99,6 @@ uint8 FAILURE_MOTOR_WARN_TEMPERATURE = 7 # (1 << 7)
|
||||
uint8 FAILURE_WARN_ESC_TEMPERATURE = 8 # (1 << 8)
|
||||
uint8 FAILURE_OVER_ESC_TEMPERATURE = 9 # (1 << 9)
|
||||
uint8 ESC_FAILURE_COUNT = 10 # Counter - keep it as last element!
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,41 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EscStatus (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EscStatus.msg)
|
||||
**TOPICS:** esc_status
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ---------------------------------------------------------- | -------------- | ---------------------------------------------------------------- | ---------- | ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| counter | `uint16` | | | incremented by the writing thread everytime new data is stored |
|
||||
| esc_count | `uint8` | | | number of connected ESCs |
|
||||
| esc_connectiontype | `uint8` | | | how ESCs connected to the system |
|
||||
| esc_online_flags | `uint8` | | | Bitmask indicating which ESC is online/offline |
|
||||
| esc_armed_flags | `uint8` | | | Bitmask indicating which ESC is armed. For ESC's where the arming state is not known (returned by the ESC), the arming bits should always be set. |
|
||||
| esc | `EscReport[8]` | | | |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| -------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ---------------------------------------------------------------------------------------------------- |
|
||||
| <a href="#CONNECTED_ESC_MAX"></a> CONNECTED_ESC_MAX | `uint8` | 8 | The number of ESCs supported. Current (Q2/2013) we support 8 ESCs |
|
||||
| <a href="#ESC_CONNECTION_TYPE_PPM"></a> ESC_CONNECTION_TYPE_PPM | `uint8` | 0 | Traditional PPM ESC |
|
||||
| <a href="#ESC_CONNECTION_TYPE_SERIAL"></a> ESC_CONNECTION_TYPE_SERIAL | `uint8` | 1 | Serial Bus connected ESC |
|
||||
| <a href="#ESC_CONNECTION_TYPE_ONESHOT"></a> ESC_CONNECTION_TYPE_ONESHOT | `uint8` | 2 | One Shot PPM |
|
||||
| <a href="#ESC_CONNECTION_TYPE_I2C"></a> ESC_CONNECTION_TYPE_I2C | `uint8` | 3 | I2C |
|
||||
| <a href="#ESC_CONNECTION_TYPE_CAN"></a> ESC_CONNECTION_TYPE_CAN | `uint8` | 4 | CAN-Bus |
|
||||
| <a href="#ESC_CONNECTION_TYPE_DSHOT"></a> ESC_CONNECTION_TYPE_DSHOT | `uint8` | 5 | DShot |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EscStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -31,5 +66,6 @@ uint8 esc_online_flags # Bitmask indicating which ESC is online/offline
|
||||
uint8 esc_armed_flags # Bitmask indicating which ESC is armed. For ESC's where the arming state is not known (returned by the ESC), the arming bits should always be set.
|
||||
|
||||
EscReport[8] esc
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,36 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorAidSource1d (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorAidSource1d.msg)
|
||||
**TOPICS:** estimator_aid_src_baro_hgt estimator_aid_src_ev_hgt estimator_aid_src_gnss_hgt estimator_aid_src_rng_hgt estimator_aid_src_airspeed estimator_aid_src_sideslip estimator_aid_src_fake_hgt estimator_aid_src_gnss_yaw estimator_aid_src_ev_yaw
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| estimator_instance | `uint8` | | | |
|
||||
| device_id | `uint32` | | | |
|
||||
| time_last_fuse | `uint64` | | | |
|
||||
| observation | `float32` | | | |
|
||||
| observation_variance | `float32` | | | |
|
||||
| innovation | `float32` | | | |
|
||||
| innovation_filtered | `float32` | | | |
|
||||
| innovation_variance | `float32` | | | |
|
||||
| test_ratio | `float32` | | | normalized innovation squared |
|
||||
| test_ratio_filtered | `float32` | | | signed filtered test ratio |
|
||||
| innovation_rejected | `bool` | | | true if the observation has been rejected |
|
||||
| fused | `bool` | | | true if the sample was successfully fused |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorAidSource1d.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -30,5 +60,6 @@ bool fused # true if the sample was successfully fused
|
||||
# TOPICS estimator_aid_src_airspeed estimator_aid_src_sideslip
|
||||
# TOPICS estimator_aid_src_fake_hgt
|
||||
# TOPICS estimator_aid_src_gnss_yaw estimator_aid_src_ev_yaw
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,36 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorAidSource2d (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorAidSource2d.msg)
|
||||
**TOPICS:** estimator_aid_src_ev_pos estimator_aid_src_fake_pos estimator_aid_src_gnss_pos estimator_aid_src_aux_global_position estimator_aid_src_aux_vel estimator_aid_src_optical_flow estimator_aid_src_drag
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| estimator_instance | `uint8` | | | |
|
||||
| device_id | `uint32` | | | |
|
||||
| time_last_fuse | `uint64` | | | |
|
||||
| observation | `float64[2]` | | | |
|
||||
| observation_variance | `float32[2]` | | | |
|
||||
| innovation | `float32[2]` | | | |
|
||||
| innovation_filtered | `float32[2]` | | | |
|
||||
| innovation_variance | `float32[2]` | | | |
|
||||
| test_ratio | `float32[2]` | | | normalized innovation squared |
|
||||
| test_ratio_filtered | `float32[2]` | | | signed filtered test ratio |
|
||||
| innovation_rejected | `bool` | | | true if the observation has been rejected |
|
||||
| fused | `bool` | | | true if the sample was successfully fused |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorAidSource2d.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -29,5 +59,6 @@ bool fused # true if the sample was successfully fused
|
||||
# TOPICS estimator_aid_src_ev_pos estimator_aid_src_fake_pos estimator_aid_src_gnss_pos estimator_aid_src_aux_global_position
|
||||
# TOPICS estimator_aid_src_aux_vel estimator_aid_src_optical_flow
|
||||
# TOPICS estimator_aid_src_drag
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,36 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorAidSource3d (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorAidSource3d.msg)
|
||||
**TOPICS:** estimator_aid_src_ev_vel estimator_aid_src_gnss_vel estimator_aid_src_gravity estimator_aid_src_mag
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| estimator_instance | `uint8` | | | |
|
||||
| device_id | `uint32` | | | |
|
||||
| time_last_fuse | `uint64` | | | |
|
||||
| observation | `float32[3]` | | | |
|
||||
| observation_variance | `float32[3]` | | | |
|
||||
| innovation | `float32[3]` | | | |
|
||||
| innovation_filtered | `float32[3]` | | | |
|
||||
| innovation_variance | `float32[3]` | | | |
|
||||
| test_ratio | `float32[3]` | | | normalized innovation squared |
|
||||
| test_ratio_filtered | `float32[3]` | | | signed filtered test ratio |
|
||||
| innovation_rejected | `bool` | | | true if the observation has been rejected |
|
||||
| fused | `bool` | | | true if the sample was successfully fused |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorAidSource3d.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -27,5 +57,6 @@ bool innovation_rejected # true if the observation has been rejected
|
||||
bool fused # true if the sample was successfully fused
|
||||
|
||||
# TOPICS estimator_aid_src_ev_vel estimator_aid_src_gnss_vel estimator_aid_src_gravity estimator_aid_src_mag
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,30 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorBias (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorBias.msg)
|
||||
**TOPICS:** estimator_baro_bias estimator_gnss_hgt_bias
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ---------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| device_id | `uint32` | | | unique device ID for the sensor that does not change between power cycles |
|
||||
| bias | `float32` | | | estimated barometric altitude bias (m) |
|
||||
| bias_var | `float32` | | | estimated barometric altitude bias variance (m^2) |
|
||||
| innov | `float32` | | | innovation of the last measurement fusion (m) |
|
||||
| innov_var | `float32` | | | innovation variance of the last measurement fusion (m^2) |
|
||||
| innov_test_ratio | `float32` | | | normalized innovation squared test ratio |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorBias.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -15,5 +39,6 @@ float32 innov_var # innovation variance of the last measurement fusion (m^2)
|
||||
float32 innov_test_ratio # normalized innovation squared test ratio
|
||||
|
||||
# TOPICS estimator_baro_bias estimator_gnss_hgt_bias
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,30 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorBias3d (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorBias3d.msg)
|
||||
**TOPICS:** estimator_bias3d estimator_ev_pos_bias
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ---------------------------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| device_id | `uint32` | | | unique device ID for the sensor that does not change between power cycles |
|
||||
| bias | `float32[3]` | | | estimated barometric altitude bias (m) |
|
||||
| bias_var | `float32[3]` | | | estimated barometric altitude bias variance (m^2) |
|
||||
| innov | `float32[3]` | | | innovation of the last measurement fusion (m) |
|
||||
| innov_var | `float32[3]` | | | innovation variance of the last measurement fusion (m^2) |
|
||||
| innov_test_ratio | `float32[3]` | | | normalized innovation squared test ratio |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorBias3d.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -17,5 +41,6 @@ float32[3] innov_test_ratio # normalized innovation squared test ratio
|
||||
|
||||
# TOPICS estimator_bias3d
|
||||
# TOPICS estimator_ev_pos_bias
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,42 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorEventFlags (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorEventFlags.msg)
|
||||
**TOPICS:** estimator_eventflags
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ----------------------------------------------------------------------------------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| information_event_changes | `uint32` | | | number of information event changes |
|
||||
| gps_checks_passed | `bool` | | | 0 - true when gps quality checks are passing passed |
|
||||
| reset_vel_to_gps | `bool` | | | 1 - true when the velocity states are reset to the gps measurement |
|
||||
| reset_vel_to_flow | `bool` | | | 2 - true when the velocity states are reset using the optical flow measurement |
|
||||
| reset_vel_to_vision | `bool` | | | 3 - true when the velocity states are reset to the vision system measurement |
|
||||
| reset_vel_to_zero | `bool` | | | 4 - true when the velocity states are reset to zero |
|
||||
| reset_pos_to_last_known | `bool` | | | 5 - true when the position states are reset to the last known position |
|
||||
| reset_pos_to_gps | `bool` | | | 6 - true when the position states are reset to the gps measurement |
|
||||
| reset_pos_to_vision | `bool` | | | 7 - true when the position states are reset to the vision system measurement |
|
||||
| starting_gps_fusion | `bool` | | | 8 - true when the filter starts using gps measurements to correct the state estimates |
|
||||
| starting_vision_pos_fusion | `bool` | | | 9 - true when the filter starts using vision system position measurements to correct the state estimates |
|
||||
| starting_vision_vel_fusion | `bool` | | | 10 - true when the filter starts using vision system velocity measurements to correct the state estimates |
|
||||
| starting_vision_yaw_fusion | `bool` | | | 11 - true when the filter starts using vision system yaw measurements to correct the state estimates |
|
||||
| yaw_aligned_to_imu_gps | `bool` | | | 12 - true when the filter resets the yaw to an estimate derived from IMU and GPS data |
|
||||
| reset_hgt_to_baro | `bool` | | | 13 - true when the vertical position state is reset to the baro measurement |
|
||||
| reset_hgt_to_gps | `bool` | | | 14 - true when the vertical position state is reset to the gps measurement |
|
||||
| reset_hgt_to_rng | `bool` | | | 15 - true when the vertical position state is reset to the rng measurement |
|
||||
| reset_hgt_to_ev | `bool` | | | 16 - true when the vertical position state is reset to the ev measurement |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorEventFlags.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -25,5 +61,6 @@ bool reset_hgt_to_baro # 13 - true when the vertical position s
|
||||
bool reset_hgt_to_gps # 14 - true when the vertical position state is reset to the gps measurement
|
||||
bool reset_hgt_to_rng # 15 - true when the vertical position state is reset to the rng measurement
|
||||
bool reset_hgt_to_ev # 16 - true when the vertical position state is reset to the ev measurement
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,39 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorGpsStatus (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorGpsStatus.msg)
|
||||
**TOPICS:** estimator_gpsstatus
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | ------------------------------------------------------------------------------------------------ |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| checks_passed | `bool` | | | |
|
||||
| check_fail_gps_fix | `bool` | | | 0 : insufficient fix type (no 3D solution) |
|
||||
| check_fail_min_sat_count | `bool` | | | 1 : minimum required sat count fail |
|
||||
| check_fail_max_pdop | `bool` | | | 2 : maximum allowed PDOP fail |
|
||||
| check_fail_max_horz_err | `bool` | | | 3 : maximum allowed horizontal position error fail |
|
||||
| check_fail_max_vert_err | `bool` | | | 4 : maximum allowed vertical position error fail |
|
||||
| check_fail_max_spd_err | `bool` | | | 5 : maximum allowed speed error fail |
|
||||
| check_fail_max_horz_drift | `bool` | | | 6 : maximum allowed horizontal position drift fail - requires stationary vehicle |
|
||||
| check_fail_max_vert_drift | `bool` | | | 7 : maximum allowed vertical position drift fail - requires stationary vehicle |
|
||||
| check_fail_max_horz_spd_err | `bool` | | | 8 : maximum allowed horizontal speed fail - requires stationary vehicle |
|
||||
| check_fail_max_vert_spd_err | `bool` | | | 9 : maximum allowed vertical velocity discrepancy fail |
|
||||
| check_fail_spoofed_gps | `bool` | | | 10 : GPS signal is spoofed |
|
||||
| position_drift_rate_horizontal_m_s | `float32` | | | Horizontal position rate magnitude (m/s) |
|
||||
| position_drift_rate_vertical_m_s | `float32` | | | Vertical position rate magnitude (m/s) |
|
||||
| filtered_horizontal_speed_m_s | `float32` | | | Filtered horizontal velocity magnitude (m/s) |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorGpsStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -23,5 +56,6 @@ bool check_fail_spoofed_gps # 10 : GPS signal is spoofed
|
||||
float32 position_drift_rate_horizontal_m_s # Horizontal position rate magnitude (m/s)
|
||||
float32 position_drift_rate_vertical_m_s # Vertical position rate magnitude (m/s)
|
||||
float32 filtered_horizontal_speed_m_s # Filtered horizontal velocity magnitude (m/s)
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,44 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorInnovations (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorInnovations.msg)
|
||||
**TOPICS:** estimator_innovations estimator_innovation_variances estimator_innovation_test_ratios
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------------------------------------------------------------------------------------------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| gps_hvel | `float32[2]` | | | horizontal GPS velocity innovation (m/sec) and innovation variance ((m/sec)\*\*2) |
|
||||
| `float32` | | | vertical GPS velocity innovation (m/sec) and innovation variance ((m/sec)\*\*2) | |
|
||||
| gps_hpos | `float32[2]` | | | horizontal GPS position innovation (m) and innovation variance (m\*\*2) |
|
||||
| `float32` | | | vertical GPS position innovation (m) and innovation variance (m\*\*2) | |
|
||||
| ev_hvel | `float32[2]` | | | horizontal external vision velocity innovation (m/sec) and innovation variance ((m/sec)\*\*2) |
|
||||
| `float32` | | | vertical external vision velocity innovation (m/sec) and innovation variance ((m/sec)\*\*2) | |
|
||||
| ev_hpos | `float32[2]` | | | horizontal external vision position innovation (m) and innovation variance (m\*\*2) |
|
||||
| `float32` | | | vertical external vision position innovation (m) and innovation variance (m\*\*2) | |
|
||||
| rng_vpos | `float32` | | | range sensor height innovation (m) and innovation variance (m\*\*2) |
|
||||
| baro_vpos | `float32` | | | barometer height innovation (m) and innovation variance (m\*\*2) |
|
||||
| aux_hvel | `float32[2]` | | | horizontal auxiliary velocity innovation from landing target measurement (m/sec) and innovation variance ((m/sec)\*\*2) |
|
||||
| flow | `float32[2]` | | | flow innvoation (rad/sec) and innovation variance ((rad/sec)\*\*2) |
|
||||
| heading | `float32` | | | heading innovation (rad) and innovation variance (rad\*\*2) |
|
||||
| mag_field | `float32[3]` | | | earth magnetic field innovation (Gauss) and innovation variance (Gauss\*\*2) |
|
||||
| gravity | `float32[3]` | | | gravity innovation from accelerometerr vector (m/s\*\*2) |
|
||||
| drag | `float32[2]` | | | drag specific force innovation (m/sec\*\*2) and innovation variance ((m/sec)\*\*2) |
|
||||
| airspeed | `float32` | | | airspeed innovation (m/sec) and innovation variance ((m/sec)\*\*2) |
|
||||
| beta | `float32` | | | synthetic sideslip innovation (rad) and innovation variance (rad\*\*2) |
|
||||
| hagl | `float32` | | | height of ground innovation (m) and innovation variance (m\*\*2) |
|
||||
| hagl_rate | `float32` | | | height of ground rate innovation (m/s) and innovation variance ((m/s)\*\*2) |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorInnovations.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -42,5 +80,6 @@ float32 hagl_rate # height of ground rate innovation (m/s) and innovation varian
|
||||
# the test ratio will be put in the first component of the vector.
|
||||
|
||||
# TOPICS estimator_innovations estimator_innovation_variances estimator_innovation_test_ratios
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,38 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorSelectorStatus (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorSelectorStatus.msg)
|
||||
**TOPICS:** estimator_selectorstatus
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ----------------------------------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| primary_instance | `uint8` | | | |
|
||||
| instances_available | `uint8` | | | |
|
||||
| instance_changed_count | `uint32` | | | |
|
||||
| last_instance_change | `uint64` | | | |
|
||||
| accel_device_id | `uint32` | | | |
|
||||
| baro_device_id | `uint32` | | | |
|
||||
| gyro_device_id | `uint32` | | | |
|
||||
| mag_device_id | `uint32` | | | |
|
||||
| combined_test_ratio | `float32[9]` | | | |
|
||||
| relative_test_ratio | `float32[9]` | | | |
|
||||
| healthy | `bool[9]` | | | |
|
||||
| accumulated_gyro_error | `float32[4]` | | | |
|
||||
| accumulated_accel_error | `float32[4]` | | | |
|
||||
| gyro_fault_detected | `bool` | | | |
|
||||
| accel_fault_detected | `bool` | | | |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorSelectorStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -25,5 +57,6 @@ float32[4] accumulated_gyro_error
|
||||
float32[4] accumulated_accel_error
|
||||
bool gyro_fault_detected
|
||||
bool accel_fault_detected
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,9 +1,44 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorSensorBias (повідомлення UORB)
|
||||
|
||||
Показання датчиків та похибки в процесі роботи в одиницях СІ. Показання датчиків компенсуються для статичних зсувів,
|
||||
похибки шкали, зсув під час роботи та тепловий зсув (якщо термокомпенсація увімкнена та доступна).
|
||||
Показання датчиків та похибки в процесі роботи в одиницях СІ. Sensor readings are compensated for static offsets,. scale errors, in-run bias and thermal drift (if thermal compensation is enabled and available).
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorSensorBias.msg)
|
||||
**TOPICS:** estimator_sensorbias
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| gyro_device_id | `uint32` | | | unique device ID for the sensor that does not change between power cycles |
|
||||
| gyro_bias | `float32[3]` | | | gyroscope in-run bias in body frame (rad/s) |
|
||||
| gyro_bias_limit | `float32` | | | magnitude of maximum gyroscope in-run bias in body frame (rad/s) |
|
||||
| gyro_bias_variance | `float32[3]` | | | |
|
||||
| gyro_bias_valid | `bool` | | | |
|
||||
| gyro_bias_stable | `bool` | | | true when the gyro bias estimate is stable enough to use for calibration |
|
||||
| accel_device_id | `uint32` | | | unique device ID for the sensor that does not change between power cycles |
|
||||
| accel_bias | `float32[3]` | | | accelerometer in-run bias in body frame (m/s^2) |
|
||||
| accel_bias_limit | `float32` | | | magnitude of maximum accelerometer in-run bias in body frame (m/s^2) |
|
||||
| accel_bias_variance | `float32[3]` | | | |
|
||||
| accel_bias_valid | `bool` | | | |
|
||||
| accel_bias_stable | `bool` | | | true when the accel bias estimate is stable enough to use for calibration |
|
||||
| mag_device_id | `uint32` | | | unique device ID for the sensor that does not change between power cycles |
|
||||
| mag_bias | `float32[3]` | | | magnetometer in-run bias in body frame (Gauss) |
|
||||
| mag_bias_limit | `float32` | | | magnitude of maximum magnetometer in-run bias in body frame (Gauss) |
|
||||
| mag_bias_variance | `float32[3]` | | | |
|
||||
| mag_bias_valid | `bool` | | | |
|
||||
| mag_bias_stable | `bool` | | | true when the mag bias estimate is stable enough to use for calibration |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorSensorBias.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
#
|
||||
@@ -36,5 +71,6 @@ float32 mag_bias_limit # magnitude of maximum magnetometer in-run bias
|
||||
float32[3] mag_bias_variance
|
||||
bool mag_bias_valid
|
||||
bool mag_bias_stable # true when the mag bias estimate is stable enough to use for calibration
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,27 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorStates (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorStates.msg)
|
||||
**TOPICS:** estimator_states
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ------------------------------------- | ------------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| states | `float32[25]` | | | Internal filter states |
|
||||
| n_states | `uint8` | | | Number of states effectively used |
|
||||
| covariances | `float32[24]` | | | Diagonal Elements of Covariance Matrix |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorStates.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -10,5 +31,6 @@ float32[25] states # Internal filter states
|
||||
uint8 n_states # Number of states effectively used
|
||||
|
||||
float32[24] covariances # Diagonal Elements of Covariance Matrix
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -1,6 +1,109 @@
|
||||
---
|
||||
pageClass: is-wide-page
|
||||
---
|
||||
|
||||
# EstimatorStatus (повідомлення UORB)
|
||||
|
||||
[source file](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorStatus.msg)
|
||||
**TOPICS:** estimator_status
|
||||
|
||||
## Fields
|
||||
|
||||
| Назва | Тип | Unit [Frame] | Range/Enum | Опис |
|
||||
| ----------------------------------------------------------------------------------------------------------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
|
||||
| output_tracking_error | `float32[3]` | | | return a vector containing the output predictor angular, velocity and position tracking error magnitudes (rad), (m/s), (m) |
|
||||
| gps_check_fail_flags | `uint16` | | | Bitmask to indicate status of GPS checks - see definition below |
|
||||
| control_mode_flags | `uint64` | | | Bitmask to indicate EKF logic state |
|
||||
| filter_fault_flags | `uint32` | | | Bitmask to indicate EKF internal faults |
|
||||
| pos_horiz_accuracy | `float32` | | | 1-Sigma estimated horizontal position accuracy relative to the estimators origin (m) |
|
||||
| pos_vert_accuracy | `float32` | | | 1-Sigma estimated vertical position accuracy relative to the estimators origin (m) |
|
||||
| hdg_test_ratio | `float32` | | | low-pass filtered ratio of the largest heading innovation component to the innovation test limit |
|
||||
| vel_test_ratio | `float32` | | | low-pass filtered ratio of the largest velocity innovation component to the innovation test limit |
|
||||
| pos_test_ratio | `float32` | | | low-pass filtered ratio of the largest horizontal position innovation component to the innovation test limit |
|
||||
| hgt_test_ratio | `float32` | | | low-pass filtered ratio of the vertical position innovation to the innovation test limit |
|
||||
| tas_test_ratio | `float32` | | | low-pass filtered ratio of the true airspeed innovation to the innovation test limit |
|
||||
| hagl_test_ratio | `float32` | | | low-pass filtered ratio of the height above ground innovation to the innovation test limit |
|
||||
| beta_test_ratio | `float32` | | | low-pass filtered ratio of the synthetic sideslip innovation to the innovation test limit |
|
||||
| solution_status_flags | `uint16` | | | Bitmask indicating which filter kinematic state outputs are valid for flight control use. |
|
||||
| reset_count_vel_ne | `uint8` | | | number of horizontal position reset events (allow to wrap if count exceeds 255) |
|
||||
| reset_count_vel_d | `uint8` | | | number of vertical velocity reset events (allow to wrap if count exceeds 255) |
|
||||
| reset_count_pos_ne | `uint8` | | | number of horizontal position reset events (allow to wrap if count exceeds 255) |
|
||||
| reset_count_pod_d | `uint8` | | | number of vertical position reset events (allow to wrap if count exceeds 255) |
|
||||
| reset_count_quat | `uint8` | | | number of quaternion reset events (allow to wrap if count exceeds 255) |
|
||||
| time_slip | `float32` | | | cumulative amount of time in seconds that the EKF inertial calculation has slipped relative to system time |
|
||||
| pre_flt_fail_innov_heading | `bool` | | | |
|
||||
| pre_flt_fail_innov_height | `bool` | | | |
|
||||
| pre_flt_fail_innov_pos_horiz | `bool` | | | |
|
||||
| pre_flt_fail_innov_vel_horiz | `bool` | | | |
|
||||
| pre_flt_fail_innov_vel_vert | `bool` | | | |
|
||||
| pre_flt_fail_mag_field_disturbed | `bool` | | | |
|
||||
| accel_device_id | `uint32` | | | |
|
||||
| gyro_device_id | `uint32` | | | |
|
||||
| baro_device_id | `uint32` | | | |
|
||||
| mag_device_id | `uint32` | | | |
|
||||
| health_flags | `uint8` | | | Bitmask to indicate sensor health states (vel, pos, hgt) |
|
||||
| timeout_flags | `uint8` | | | Bitmask to indicate timeout flags (vel, pos, hgt) |
|
||||
| mag_inclination_deg | `float32` | | | |
|
||||
| mag_inclination_ref_deg | `float32` | | | |
|
||||
| mag_strength_gs | `float32` | | | |
|
||||
| mag_strength_ref_gs | `float32` | | | |
|
||||
|
||||
## Constants
|
||||
|
||||
| Назва | Тип | Значення | Опис |
|
||||
| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | -------- | ------------------------------------------------------------------------------------------------- |
|
||||
| <a href="#GPS_CHECK_FAIL_GPS_FIX"></a> GPS_CHECK_FAIL_GPS_FIX | `uint8` | 0 | 0 : insufficient fix type (no 3D solution) |
|
||||
| <a href="#GPS_CHECK_FAIL_MIN_SAT_COUNT"></a> GPS_CHECK_FAIL_MIN_SAT_COUNT | `uint8` | 1 | 1 : minimum required sat count fail |
|
||||
| <a href="#GPS_CHECK_FAIL_MAX_PDOP"></a> GPS_CHECK_FAIL_MAX_PDOP | `uint8` | 2 | 2 : maximum allowed PDOP fail |
|
||||
| <a href="#GPS_CHECK_FAIL_MAX_HORZ_ERR"></a> GPS_CHECK_FAIL_MAX_HORZ_ERR | `uint8` | 3 | 3 : maximum allowed horizontal position error fail |
|
||||
| <a href="#GPS_CHECK_FAIL_MAX_VERT_ERR"></a> GPS_CHECK_FAIL_MAX_VERT_ERR | `uint8` | 4 | 4 : maximum allowed vertical position error fail |
|
||||
| <a href="#GPS_CHECK_FAIL_MAX_SPD_ERR"></a> GPS_CHECK_FAIL_MAX_SPD_ERR | `uint8` | 5 | 5 : maximum allowed speed error fail |
|
||||
| <a href="#GPS_CHECK_FAIL_MAX_HORZ_DRIFT"></a> GPS_CHECK_FAIL_MAX_HORZ_DRIFT | `uint8` | 6 | 6 : maximum allowed horizontal position drift fail - requires stationary vehicle |
|
||||
| <a href="#GPS_CHECK_FAIL_MAX_VERT_DRIFT"></a> GPS_CHECK_FAIL_MAX_VERT_DRIFT | `uint8` | 7 | 7 : maximum allowed vertical position drift fail - requires stationary vehicle |
|
||||
| <a href="#GPS_CHECK_FAIL_MAX_HORZ_SPD_ERR"></a> GPS_CHECK_FAIL_MAX_HORZ_SPD_ERR | `uint8` | 8 | 8 : maximum allowed horizontal speed fail - requires stationary vehicle |
|
||||
| <a href="#GPS_CHECK_FAIL_MAX_VERT_SPD_ERR"></a> GPS_CHECK_FAIL_MAX_VERT_SPD_ERR | `uint8` | 9 | 9 : maximum allowed vertical velocity discrepancy fail |
|
||||
| <a href="#GPS_CHECK_FAIL_SPOOFED"></a> GPS_CHECK_FAIL_SPOOFED | `uint8` | 10 | 10 : GPS signal is spoofed |
|
||||
| <a href="#GPS_CHECK_FAIL_JAMMED"></a> GPS_CHECK_FAIL_JAMMED | `uint8` | 11 | 11 : GPS signal is jammed |
|
||||
| <a href="#CS_TILT_ALIGN"></a> CS_TILT_ALIGN | `uint8` | 0 | 0 - true if the filter tilt alignment is complete |
|
||||
| <a href="#CS_YAW_ALIGN"></a> CS_YAW_ALIGN | `uint8` | 1 | 1 - true if the filter yaw alignment is complete |
|
||||
| <a href="#CS_GNSS_POS"></a> CS_GNSS_POS | `uint8` | 2 | 2 - true if GNSS position measurements are being fused |
|
||||
| <a href="#CS_OPT_FLOW"></a> CS_OPT_FLOW | `uint8` | 3 | 3 - true if optical flow measurements are being fused |
|
||||
| <a href="#CS_MAG_HDG"></a> CS_MAG_HDG | `uint8` | 4 | 4 - true if a simple magnetic yaw heading is being fused |
|
||||
| <a href="#CS_MAG_3D"></a> CS_MAG_3D | `uint8` | 5 | 5 - true if 3-axis magnetometer measurement are being fused |
|
||||
| <a href="#CS_MAG_DEC"></a> CS_MAG_DEC | `uint8` | 6 | 6 - true if synthetic magnetic declination measurements are being fused |
|
||||
| <a href="#CS_IN_AIR"></a> CS_IN_AIR | `uint8` | 7 | 7 - true when thought to be airborne |
|
||||
| <a href="#CS_WIND"></a> CS_WIND | `uint8` | 8 | 8 - true when wind velocity is being estimated |
|
||||
| <a href="#CS_BARO_HGT"></a> CS_BARO_HGT | `uint8` | 9 | 9 - true when baro data is being fused |
|
||||
| <a href="#CS_RNG_HGT"></a> CS_RNG_HGT | `uint8` | 10 | 10 - true when range finder data is being fused for height aiding |
|
||||
| <a href="#CS_GPS_HGT"></a> CS_GPS_HGT | `uint8` | 11 | 11 - true when GPS altitude is being fused |
|
||||
| <a href="#CS_EV_POS"></a> CS_EV_POS | `uint8` | 12 | 12 - true when local position data from external vision is being fused |
|
||||
| <a href="#CS_EV_YAW"></a> CS_EV_YAW | `uint8` | 13 | 13 - true when yaw data from external vision measurements is being fused |
|
||||
| <a href="#CS_EV_HGT"></a> CS_EV_HGT | `uint8` | 14 | 14 - true when height data from external vision measurements is being fused |
|
||||
| <a href="#CS_BETA"></a> CS_BETA | `uint8` | 15 | 15 - true when synthetic sideslip measurements are being fused |
|
||||
| <a href="#CS_MAG_FIELD"></a> CS_MAG_FIELD | `uint8` | 16 | 16 - true when only the magnetic field states are updated by the magnetometer |
|
||||
| <a href="#CS_FIXED_WING"></a> CS_FIXED_WING | `uint8` | 17 | 17 - true when thought to be operating as a fixed wing vehicle with constrained sideslip |
|
||||
| <a href="#CS_MAG_FAULT"></a> CS_MAG_FAULT | `uint8` | 18 | 18 - true when the magnetometer has been declared faulty and is no longer being used |
|
||||
| <a href="#CS_ASPD"></a> CS_ASPD | `uint8` | 19 | 19 - true when airspeed measurements are being fused |
|
||||
| <a href="#CS_GND_EFFECT"></a> CS_GND_EFFECT | `uint8` | 20 | 20 - true when when protection from ground effect induced static pressure rise is active |
|
||||
| <a href="#CS_RNG_STUCK"></a> CS_RNG_STUCK | `uint8` | 21 | 21 - true when a stuck range finder sensor has been detected |
|
||||
| <a href="#CS_GPS_YAW"></a> CS_GPS_YAW | `uint8` | 22 | 22 - true when yaw (not ground course) data from a GPS receiver is being fused |
|
||||
| <a href="#CS_MAG_ALIGNED"></a> CS_MAG_ALIGNED | `uint8` | 23 | 23 - true when the in-flight mag field alignment has been completed |
|
||||
| <a href="#CS_EV_VEL"></a> CS_EV_VEL | `uint8` | 24 | 24 - true when local frame velocity data fusion from external vision measurements is intended |
|
||||
| <a href="#CS_SYNTHETIC_MAG_Z"></a> CS_SYNTHETIC_MAG_Z | `uint8` | 25 | 25 - true when we are using a synthesized measurement for the magnetometer Z component |
|
||||
| <a href="#CS_VEHICLE_AT_REST"></a> CS_VEHICLE_AT_REST | `uint8` | 26 | 26 - true when the vehicle is at rest |
|
||||
| <a href="#CS_GPS_YAW_FAULT"></a> CS_GPS_YAW_FAULT | `uint8` | 27 | 27 - true when the GNSS heading has been declared faulty and is no longer being used |
|
||||
| <a href="#CS_RNG_FAULT"></a> CS_RNG_FAULT | `uint8` | 28 | 28 - true when the range finder has been declared faulty and is no longer being used |
|
||||
| <a href="#CS_GNSS_VEL"></a> CS_GNSS_VEL | `uint8` | 44 | 44 - true if GNSS velocity measurement fusion is intended |
|
||||
| <a href="#CS_GNSS_FAULT"></a> CS_GNSS_FAULT | `uint8` | 45 | 45 - true if GNSS measurements have been declared faulty and are no longer used |
|
||||
| <a href="#CS_YAW_MANUAL"></a> CS_YAW_MANUAL | `uint8` | 46 | 46 - true if yaw has been set manually |
|
||||
|
||||
## Source Message
|
||||
|
||||
[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/EstimatorStatus.msg)
|
||||
|
||||
:::details
|
||||
Click here to see original file
|
||||
|
||||
```c
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
@@ -130,5 +233,6 @@ float32 mag_inclination_deg
|
||||
float32 mag_inclination_ref_deg
|
||||
float32 mag_strength_gs
|
||||
float32 mag_strength_ref_gs
|
||||
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
Some files were not shown because too many files have changed in this diff Show More
Reference in New Issue
Block a user